Started by upstream project "ESP_RegCaps" build number 671
originally caused by:
Started by an SCM change
Running as SYSTEM
[EnvInject] - Loading node environment variables.
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A training/lectures
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A training/lectures/session02.tex
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A training/lectures/Makefile
A training/lectures/muddy_06_07.tex
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A training/lectures/session10
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A training/lectures/CAPSflyer.tex
A training/lectures/session04.tex
A training/lectures/welcome
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A training/lectures/session04
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A training/lectures/csmListing.tex
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A training/lectures/session01
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A training/lectures/session08
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AU training/lectures/cmpress
A training/lectures/PythonTutorial.tex
A training/lectures/session02
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A training/lectures/session03
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A training/lectures/capsSyllabus.tex
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AU training/lectures/questionnaire.docx
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A training/lectures/ParaviewBasics
AU training/lectures/ParaviewBasics/basic_paraview.pdf
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A training/lectures/BEAMERoptions.tex
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A training/lectures/beamercolorthemeesp.sty
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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 2511
Cleaning up /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM
Deleting /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM/pyOCSM/__pycache__
Updating svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/pyOCSM at revision '2024-07-11T22:19:11.168 -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 2511
No changes for svn+ssh://acdl.mit.edu/home/svnroot/EGADS since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/CAPS 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’
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 [viggen] is in [[macys, macys_VM, reynolds, viggen]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[DARWIN_ARM64] $ /bin/bash -xe /var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jenkins3237286271013217037.sh
+ rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training/lectures
+ [[ CAPS/unit != *\S\l\u\g\s* ]]
+ rm -rf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/data/Slugs
+ [[ viggen == *\v\i\g\g\e\n* ]]
+ arch -arch arm64 /bin/bash -ex /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/ESP_Regression.sh
+ source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ viggen == \r\e\y\n\o\l\d\s ]]
++ [[ DARWIN_ARM64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /Users/jenkins/.bashrc ']'
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ export ESP_UDC_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/personalUdc
++ ESP_UDC_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/personalUdc
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_BLOC=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64
++ ESP_ROOT=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64
++ export JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ JULIA_DEPOT_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ viggen == *\r\e\y\n\o\l\d\s* ]]
++ [[ viggen == *\m\a\c\y\s* ]]
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export EMPnumProc=2
++ EMPnumProc=2
++ export OMP_NUM_THREADS=2
++ OMP_NUM_THREADS=2
++ source /Users/jenkins/.bash_profile
++++ /opt/homebrew/bin/brew shellenv
+++ eval 'export HOMEBREW_PREFIX="/opt/homebrew";
export HOMEBREW_CELLAR="/opt/homebrew/Cellar";
export HOMEBREW_REPOSITORY="/opt/homebrew";
export PATH="/opt/homebrew/bin:/opt/homebrew/sbin${PATH+:$PATH}";
export MANPATH="/opt/homebrew/share/man${MANPATH+:$MANPATH}:";
export INFOPATH="/opt/homebrew/share/info:${INFOPATH:-}";'
++++ export HOMEBREW_PREFIX=/opt/homebrew
++++ HOMEBREW_PREFIX=/opt/homebrew
++++ export HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ HOMEBREW_CELLAR=/opt/homebrew/Cellar
++++ export HOMEBREW_REPOSITORY=/opt/homebrew
++++ HOMEBREW_REPOSITORY=/opt/homebrew
++++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin
++++ export MANPATH=/opt/homebrew/share/man:
++++ MANPATH=/opt/homebrew/share/man:
++++ export INFOPATH=/opt/homebrew/share/info:
++++ INFOPATH=/opt/homebrew/share/info:
+++ [[ -r /opt/homebrew/etc/profile.d/bash_completion.sh ]]
+++ . /opt/homebrew/etc/profile.d/bash_completion.sh
++++ '[' -z '3.2.57(1)-release' -o -z '' -o -n '' ']'
++++ return
+++ export NETCDF_PATH=/opt/homebrew
+++ NETCDF_PATH=/opt/homebrew
++ [[ viggen == *\m\a\c\y\s* ]]
++ export PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ export CASARCH=.
++ CASARCH=.
++ '[' '!' -z '' ']'
+++ ls -d /Users/jenkins/util/ESP/OpenCASCADE-7.8.0
++ 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/DARWIN_ARM64/ESP/udunits/udunits2.xml
++ UDUNITS2_XML_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/udunits/udunits2.xml
++ export ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/Users/jenkins/util/ESP/ExternLibs
++ export DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ DYLD_LIBRARY_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib:/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/opt/intel/oneapi/tbb/2021.5.0/env/../lib:/opt/intel/oneapi/mkl/2022.0.0/lib
++ export AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/Users/jenkins/util/AFLR/aflr_lib_11.5.14
++ [[ viggen == *\m\a\c\y\s* ]]
++ export AFLR_ARCH=MacOSX-arm64
++ AFLR_ARCH=MacOSX-arm64
++ export ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ ASTROS_ROOT=/Users/jenkins/util/astros/Astros/Darwin-64bit
++ export PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ CART3D=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16
++ export CART3D_ARCH=OSX64_ICC
++ CART3D_ARCH=OSX64_ICC
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ export VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ VSP3_ROOT=/Users/jenkins/util/OpenVSP/OpenVSP-3.38.0-MacOS
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export SEACAS=/Users/jenkins/util/sandialabs/seacas
++ SEACAS=/Users/jenkins/util/sandialabs/seacas
++ [[ viggen == \v\i\g\g\e\n ]]
++ export NETCDFINC=/opt/homebrew/include
++ NETCDFINC=/opt/homebrew/include
++ export SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/Users/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/Users/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16 ']'
+++ perl -I/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
++ eval 'PATH="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/pyCAPS:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/pyOCSM:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/pyEGADS::/Users/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ viggen == \m\a\c\y\s* ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ rm -f /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-*'
++ rm -f '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-*'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/python3-config /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/virtualenv /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/virtualenv
+++ ls /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-build /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-c++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/analyze-cc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/analyze-cc
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-build /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-build
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-c++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-c++
++ for i in '`ls /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/analyze-* /Users/jenkins/util/ESP/Python/ESP_Python-${PYTHON_VERSION}/bin/intercept-*`'
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
+++ basename /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc
++ ln -s /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin/intercept-cc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/intercept-cc
+++ python-config --includes
++ export 'PYTHONINC=. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/python-config [--prefix|--exec-prefix|--includes|--libs|--cflags|--ldflags|--extension-suffix|--help|--abiflags|--configdir|--embed] == *\e\m\b\e\d* ]]
+++ python-config --ldflags --embed
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation'
++ [[ viggen == \m\a\c\y\s ]]
++ [[ viggen == \v\i\g\g\e\n ]]
++ export 'PYTHONLIB=-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ PYTHONLIB='-L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w'
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ DARWIN_ARM64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/data
++ CSMDATA=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/data
+ source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/ESPbfr.sh
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/
++ tar -xvf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/ESPbfr.tgz
x ESP/
x ESP/CYGWIN64/
x ESP/CYGWIN64/bin/
x ESP/CYGWIN64/bin/mastros.exe
x ESP/CYGWIN64/bin/ASTRO.D01
x ESP/CYGWIN64/bin/ASTRO.IDX
x ESP/CYGWIN64/include/
x ESP/CYGWIN64/lib/
x ESP/CYGWIN64/lib/libquadmath-0.dll
x ESP/CYGWIN64/lib/libwinpthread-1.dll
x ESP/CYGWIN64/lib/libgcc_s_sjlj-1.dll
x ESP/CYGWIN64/obj/
x ESP/CYGWIN64/test/
x ESP/DARWIN64/
x ESP/DARWIN64/bin/
x ESP/DARWIN64/bin/mastros.exe
x ESP/DARWIN64/bin/ASTRO.D01
x ESP/DARWIN64/bin/mset
x ESP/DARWIN64/bin/ASTRO.IDX
x ESP/DARWIN64/bin/avl
x ESP/DARWIN64/bin/xfoil
x ESP/DARWIN64/bin/mses
x ESP/DARWIN64/include/
x ESP/DARWIN64/include/nmb.h
x ESP/DARWIN64/include/xddm/
x ESP/DARWIN64/include/xddm/xddmInternals.h
x ESP/DARWIN64/include/xddm/xddm.h
x ESP/DARWIN64/include/xddm/xddm.c
x ESP/DARWIN64/include/converter.h
x ESP/DARWIN64/include/libCart3D/
x ESP/DARWIN64/include/libCart3D/sensors.h
x ESP/DARWIN64/include/libCart3D/SFC.h
x ESP/DARWIN64/include/libCart3D/map.h
x ESP/DARWIN64/include/libCart3D/MGinfo.h
x ESP/DARWIN64/include/libCart3D/gridStructures.h
x ESP/DARWIN64/include/libCart3D/timer.h
x ESP/DARWIN64/include/libCart3D/ConvInfo.h
x ESP/DARWIN64/include/libCart3D/dualtime.h
x ESP/DARWIN64/include/libCart3D/stateVector.h
x ESP/DARWIN64/include/libCart3D/cartCells.h
x ESP/DARWIN64/include/libCart3D/encoding.h
x ESP/DARWIN64/include/libCart3D/string_util.h
x ESP/DARWIN64/include/libCart3D/int64.h
x ESP/DARWIN64/include/libCart3D/bBox_stuff.h
x ESP/DARWIN64/include/libCart3D/basicTypes.h
x ESP/DARWIN64/include/libCart3D/utils_xml.h
x ESP/DARWIN64/include/libCart3D/hex.h
x ESP/DARWIN64/include/libCart3D/PostProcInfo.h
x ESP/DARWIN64/include/libCart3D/SolverInfo.h
x ESP/DARWIN64/include/libCart3D/earthBL_BC.h
x ESP/DARWIN64/include/libCart3D/limiters.h
x ESP/DARWIN64/include/libCart3D/geomStructures.h
x ESP/DARWIN64/include/libCart3D/CaseInfo.h
x ESP/DARWIN64/include/libCart3D/memory_util.h
x ESP/DARWIN64/include/libCart3D/infoStructures.h
x ESP/DARWIN64/include/libCart3D/geomTypes.h
x ESP/DARWIN64/include/libCart3D/c3d_timeout.h
x ESP/DARWIN64/include/libCart3D/myLList.h
x ESP/DARWIN64/include/libCart3D/IOinfo.h
x ESP/DARWIN64/include/libCart3D/GridInfo.h
x ESP/DARWIN64/include/libCart3D/c3d_global.h
x ESP/DARWIN64/include/libCart3D/vortexBC.h
x ESP/DARWIN64/include/c3dio/
x ESP/DARWIN64/include/c3dio/c3dio_icemcfd.h
x ESP/DARWIN64/include/c3dio/c3dio_lib.h
x ESP/DARWIN64/include/udunits.h
x ESP/DARWIN64/include/udunits2.h
x ESP/DARWIN64/lib/
x ESP/DARWIN64/lib/libudunits2.dylib
x ESP/DARWIN64/lib/libudunits2.0.dylib
x ESP/DARWIN64/lib/libCart3D.a
x ESP/DARWIN64/lib/libnmb.dylib
x ESP/DARWIN64/lib/libc3dio.a
x ESP/DARWIN64/obj/
x ESP/DARWIN64/test/
x ESP/DARWIN_ARM64/
x ESP/DARWIN_ARM64/bin/
x ESP/DARWIN_ARM64/bin/mastros.exe
x ESP/DARWIN_ARM64/bin/ASTRO.D01
x ESP/DARWIN_ARM64/bin/mset
x ESP/DARWIN_ARM64/bin/ASTRO.IDX
x ESP/DARWIN_ARM64/bin/avl
x ESP/DARWIN_ARM64/bin/xfoil
x ESP/DARWIN_ARM64/bin/mses
x ESP/DARWIN_ARM64/include/
x ESP/DARWIN_ARM64/include/nmb.h
x ESP/DARWIN_ARM64/include/xddm/
x ESP/DARWIN_ARM64/include/xddm/xddmInternals.h
x ESP/DARWIN_ARM64/include/xddm/xddm.h
x ESP/DARWIN_ARM64/include/xddm/xddm.c
x ESP/DARWIN_ARM64/include/converter.h
x ESP/DARWIN_ARM64/include/libCart3D/
x ESP/DARWIN_ARM64/include/libCart3D/sensors.h
x ESP/DARWIN_ARM64/include/libCart3D/SFC.h
x ESP/DARWIN_ARM64/include/libCart3D/map.h
x ESP/DARWIN_ARM64/include/libCart3D/MGinfo.h
x ESP/DARWIN_ARM64/include/libCart3D/gridStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/timer.h
x ESP/DARWIN_ARM64/include/libCart3D/ConvInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/dualtime.h
x ESP/DARWIN_ARM64/include/libCart3D/stateVector.h
x ESP/DARWIN_ARM64/include/libCart3D/cartCells.h
x ESP/DARWIN_ARM64/include/libCart3D/encoding.h
x ESP/DARWIN_ARM64/include/libCart3D/string_util.h
x ESP/DARWIN_ARM64/include/libCart3D/int64.h
x ESP/DARWIN_ARM64/include/libCart3D/bBox_stuff.h
x ESP/DARWIN_ARM64/include/libCart3D/basicTypes.h
x ESP/DARWIN_ARM64/include/libCart3D/utils_xml.h
x ESP/DARWIN_ARM64/include/libCart3D/hex.h
x ESP/DARWIN_ARM64/include/libCart3D/PostProcInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/SolverInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/earthBL_BC.h
x ESP/DARWIN_ARM64/include/libCart3D/limiters.h
x ESP/DARWIN_ARM64/include/libCart3D/geomStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/CaseInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/memory_util.h
x ESP/DARWIN_ARM64/include/libCart3D/infoStructures.h
x ESP/DARWIN_ARM64/include/libCart3D/geomTypes.h
x ESP/DARWIN_ARM64/include/libCart3D/c3d_timeout.h
x ESP/DARWIN_ARM64/include/libCart3D/myLList.h
x ESP/DARWIN_ARM64/include/libCart3D/IOinfo.h
x ESP/DARWIN_ARM64/include/libCart3D/GridInfo.h
x ESP/DARWIN_ARM64/include/libCart3D/c3d_global.h
x ESP/DARWIN_ARM64/include/libCart3D/vortexBC.h
x ESP/DARWIN_ARM64/include/c3dio/
x ESP/DARWIN_ARM64/include/c3dio/c3dio_icemcfd.h
x ESP/DARWIN_ARM64/include/c3dio/c3dio_lib.h
x ESP/DARWIN_ARM64/include/udunits.h
x ESP/DARWIN_ARM64/include/udunits2.h
x ESP/DARWIN_ARM64/lib/
x ESP/DARWIN_ARM64/lib/libudunits2.dylib
x ESP/DARWIN_ARM64/lib/libudunits2.0.dylib
x ESP/DARWIN_ARM64/lib/libCart3D.a
x ESP/DARWIN_ARM64/lib/libc3dio.a
x ESP/DARWIN_ARM64/obj/
x ESP/DARWIN_ARM64/test/
x ESP/LINUX64/
x ESP/LINUX64/bin/
x ESP/LINUX64/bin/mastros.exe
x ESP/LINUX64/bin/ASTRO.D01
x ESP/LINUX64/bin/mset
x ESP/LINUX64/bin/ASTRO.IDX
x ESP/LINUX64/bin/avl
x ESP/LINUX64/bin/xfoil
x ESP/LINUX64/bin/mses
x ESP/LINUX64/include/
x ESP/LINUX64/include/nmb.h
x ESP/LINUX64/include/xddm/
x ESP/LINUX64/include/xddm/xddmInternals.h
x ESP/LINUX64/include/xddm/xddm.h
x ESP/LINUX64/include/xddm/xddm.c
x ESP/LINUX64/include/libCart3D/
x ESP/LINUX64/include/libCart3D/sensors.h
x ESP/LINUX64/include/libCart3D/SFC.h
x ESP/LINUX64/include/libCart3D/map.h
x ESP/LINUX64/include/libCart3D/MGinfo.h
x ESP/LINUX64/include/libCart3D/gridStructures.h
x ESP/LINUX64/include/libCart3D/timer.h
x ESP/LINUX64/include/libCart3D/ConvInfo.h
x ESP/LINUX64/include/libCart3D/dualtime.h
x ESP/LINUX64/include/libCart3D/stateVector.h
x ESP/LINUX64/include/libCart3D/cartCells.h
x ESP/LINUX64/include/libCart3D/encoding.h
x ESP/LINUX64/include/libCart3D/string_util.h
x ESP/LINUX64/include/libCart3D/int64.h
x ESP/LINUX64/include/libCart3D/bBox_stuff.h
x ESP/LINUX64/include/libCart3D/basicTypes.h
x ESP/LINUX64/include/libCart3D/utils_xml.h
x ESP/LINUX64/include/libCart3D/hex.h
x ESP/LINUX64/include/libCart3D/PostProcInfo.h
x ESP/LINUX64/include/libCart3D/SolverInfo.h
x ESP/LINUX64/include/libCart3D/earthBL_BC.h
x ESP/LINUX64/include/libCart3D/limiters.h
x ESP/LINUX64/include/libCart3D/geomStructures.h
x ESP/LINUX64/include/libCart3D/CaseInfo.h
x ESP/LINUX64/include/libCart3D/memory_util.h
x ESP/LINUX64/include/libCart3D/infoStructures.h
x ESP/LINUX64/include/libCart3D/geomTypes.h
x ESP/LINUX64/include/libCart3D/c3d_timeout.h
x ESP/LINUX64/include/libCart3D/myLList.h
x ESP/LINUX64/include/libCart3D/IOinfo.h
x ESP/LINUX64/include/libCart3D/GridInfo.h
x ESP/LINUX64/include/libCart3D/c3d_global.h
x ESP/LINUX64/include/libCart3D/vortexBC.h
x ESP/LINUX64/include/c3dio/
x ESP/LINUX64/include/c3dio/c3dio_icemcfd.h
x ESP/LINUX64/include/c3dio/c3dio_lib.h
x ESP/LINUX64/lib/
x ESP/LINUX64/lib/libnmb.so
x ESP/LINUX64/lib/libCart3D.a
x ESP/LINUX64/lib/libc3dio.a
x ESP/LINUX64/obj/
x ESP/LINUX64/test/
x ESP/WIN64/
x ESP/WIN64/bin/
x ESP/WIN64/bin/mses.exe
x ESP/WIN64/bin/avl.exe
x ESP/WIN64/bin/mastros.exe
x ESP/WIN64/bin/ASTRO.D01
x ESP/WIN64/bin/xfoil.exe
x ESP/WIN64/bin/ASTRO.IDX
x ESP/WIN64/bin/mset.exe
x ESP/WIN64/include/
x ESP/WIN64/include/nmb.h
x ESP/WIN64/include/winhelpers/
x ESP/WIN64/include/winhelpers/gettimeofday.h
x ESP/WIN64/include/winhelpers/websock-w32.h
x ESP/WIN64/include/winhelpers/netdb.h
x ESP/WIN64/include/winhelpers/unistd.h
x ESP/WIN64/include/winhelpers/strings.h
x ESP/WIN64/include/winhelpers/sys/
x ESP/WIN64/include/winhelpers/sys/time.h
x ESP/WIN64/include/converter.h
x ESP/WIN64/include/udunits.h
x ESP/WIN64/include/udunits2.h
x ESP/WIN64/lib/
x ESP/WIN64/lib/libquadmath-0.dll
x ESP/WIN64/lib/nmb.lib
x ESP/WIN64/lib/libwinpthread-1.dll
x ESP/WIN64/lib/udunits2.lib
x ESP/WIN64/lib/libgcc_s_sjlj-1.dll
x ESP/WIN64/lib/expat.dll
x ESP/WIN64/lib/udunits2.dll
x ESP/WIN64/lib/nmb.dll
x ESP/WIN64/obj/
x ESP/WIN64/test/
x ESP/LINUX_AARCH64/
x ESP/LINUX_AARCH64/bin/
x ESP/LINUX_AARCH64/bin/mastros.exe
x ESP/LINUX_AARCH64/bin/ASTRO.D01
x ESP/LINUX_AARCH64/bin/mset
x ESP/LINUX_AARCH64/bin/ASTRO.IDX
x ESP/LINUX_AARCH64/bin/avl
x ESP/LINUX_AARCH64/bin/xfoil
x ESP/LINUX_AARCH64/bin/mses
x ESP/LINUX_AARCH64/include/
x ESP/LINUX_AARCH64/lib/
x ESP/LINUX_AARCH64/obj/
x ESP/LINUX_AARCH64/test/
x ESP/udunits/
x ESP/udunits/udunits2-accepted.xml
x ESP/udunits/udunits2-base.xml
x ESP/udunits/udunits2-common.xml
x ESP/udunits/udunits2.xml
x ESP/udunits/udunits2-derived.xml
x ESP/udunits/udunits2-prefixes.xml
++ virtualenv --system-site-packages /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
created virtual environment CPython3.11.9.final.0-64 in 439ms
creator CPython3Posix(dest=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv, clear=False, no_vcs_ignore=False, global=True)
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==70.0.0, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
++ . /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/activate
+++ '[' /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/activate = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/ESP_Regression.sh ']'
+++ deactivate nondestructive
+++ unset -f pydoc
+++ '[' -z '' ']'
+++ '[' -z '' ']'
+++ hash -r
+++ '[' -z '' ']'
+++ unset VIRTUAL_ENV
+++ unset VIRTUAL_ENV_PROMPT
+++ '[' '!' nondestructive = nondestructive ']'
+++ VIRTUAL_ENV=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
+++ '[' darwin23 = cygwin ']'
+++ '[' darwin23 = msys ']'
+++ export VIRTUAL_ENV
+++ _OLD_VIRTUAL_PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ PATH=/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test:/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/lib/perl/bin:/Users/jenkins/util/tsfoil:/Users/jenkins/util/refine/build_parallel/install/bin:/Users/jenkins/util/delaundo/delaundo/src:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin:/Users/jenkins/util/cart3d/cart3d_v1.5.9_OSX64_ICC--22.11.16/bin/OSX64_ICC/:/Users/jenkins/util/astros/Astros/Darwin-64bit:/opt/homebrew/bin:/opt/homebrew/sbin:/opt/intel/oneapi/dev-utilities/2021.5.0/bin:/usr/bin:/bin:/usr/sbin:/sbin:/opt/homebrew/bin/:/Users/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ '[' x '!=' x ']'
++++ basename /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
+++ VIRTUAL_ENV_PROMPT=venv
+++ export VIRTUAL_ENV_PROMPT
+++ '[' -z '' ']'
+++ '[' -z '' ']'
+++ _OLD_VIRTUAL_PS1=
+++ PS1='(venv) '
+++ export PS1
+++ alias pydoc
+++ true
+++ hash -r
++ pip_install pip
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP/venv/lib/python3.11/site-packages (24.0)
Collecting pip
Using cached pip-24.1.2-py3-none-any.whl.metadata (3.6 kB)
Using cached pip-24.1.2-py3-none-any.whl (1.8 MB)
Installing collected packages: pip
Attempting uninstall: pip
Found existing installation: pip 24.0
Uninstalling pip-24.0:
Successfully uninstalled pip-24.0
Successfully installed pip-24.1.2
++ pip_install f90nml
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade f90nml
Requirement already satisfied: f90nml in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.4.4)
++ pip_install numpy
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade numpy
Requirement already satisfied: numpy in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.26.4)
Collecting numpy
Using cached numpy-2.0.0-cp311-cp311-macosx_14_0_arm64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-macosx_14_0_arm64.whl (5.2 MB)
Installing collected packages: numpy
Attempting uninstall: numpy
Found existing installation: numpy 1.26.4
Not uninstalling numpy at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
Can't uninstall 'numpy'. No files were found to uninstall.
ERROR: pip's dependency resolver does not currently take into account all the packages that are installed. This behaviour is the source of the following dependency conflicts.
openmdao 3.33.0 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
pynastran 1.4.1 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
tacs 3.7.2 requires numpy<2.0.0, but you have numpy 2.0.0 which is incompatible.
Successfully installed numpy-2.0.0
++ pip_install 'scipy!=1.9.2,!=1.9.3'
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade 'scipy!=1.9.2,!=1.9.3'
Requirement already satisfied: scipy!=1.9.2,!=1.9.3 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.13.1)
Collecting scipy!=1.9.2,!=1.9.3
Using cached scipy-1.14.0-cp311-cp311-macosx_14_0_arm64.whl.metadata (60 kB)
Requirement already satisfied: numpy<2.3,>=1.23.5 in ./ESP/venv/lib/python3.11/site-packages (from scipy!=1.9.2,!=1.9.3) (2.0.0)
Using cached scipy-1.14.0-cp311-cp311-macosx_14_0_arm64.whl (23.1 MB)
Installing collected packages: scipy
Attempting uninstall: scipy
Found existing installation: scipy 1.13.1
Not uninstalling scipy at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
Can't uninstall 'scipy'. No files were found to uninstall.
ERROR: pip's dependency resolver does not currently take into account all the packages that are installed. This behaviour is the source of the following dependency conflicts.
openmdao 3.33.0 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
pynastran 1.4.1 requires numpy<2, but you have numpy 2.0.0 which is incompatible.
tacs 3.7.2 requires numpy<2.0.0, but you have numpy 2.0.0 which is incompatible.
Successfully installed scipy-1.14.0
++ pip_install openmdao
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade openmdao
Requirement already satisfied: openmdao in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.33.0)
Requirement already satisfied: networkx>=2.0 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (3.3)
Collecting numpy<2 (from openmdao)
Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl.metadata (114 kB)
Requirement already satisfied: packaging in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (24.1)
Requirement already satisfied: requests in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from openmdao) (2.32.3)
Requirement already satisfied: scipy in ./ESP/venv/lib/python3.11/site-packages (from openmdao) (1.14.0)
Requirement already satisfied: charset-normalizer<4,>=2 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (3.3.2)
Requirement already satisfied: idna<4,>=2.5 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (3.7)
Requirement already satisfied: urllib3<3,>=1.21.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (2.2.2)
Requirement already satisfied: certifi>=2017.4.17 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from requests->openmdao) (2024.6.2)
Using cached numpy-1.26.4-cp311-cp311-macosx_11_0_arm64.whl (14.0 MB)
Installing collected packages: numpy
Attempting uninstall: numpy
Found existing installation: numpy 2.0.0
Uninstalling numpy-2.0.0:
Successfully uninstalled numpy-2.0.0
Successfully installed numpy-1.26.4
++ [[ viggen == *\v\i\g\g\e\n* ]]
++ export CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
++ CVXOPT_BLAS_LIB_DIR=/Users/acdl/workspace/ESP/Python/lapack-3.10.1/build/lib
++ export CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
++ CVXOPT_SUITESPARSE_SRC_DIR=/Users/acdl/workspace/ESP/Python/SuiteSparse-5.12.0
++ GCC_MAJOR=12
++ export 'CVXOPT_BLAS_EXTRA_LINK_ARGS=/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a'
++ CVXOPT_BLAS_EXTRA_LINK_ARGS='/opt/homebrew/opt/gcc/lib/gcc/current/libgfortran.a;/opt/homebrew/opt/gcc/lib/gcc/current/libquadmath.a;/opt/homebrew/opt/gcc/lib/gcc/current/gcc/aarch64-apple-darwin21/12/libgcc.a'
++ pip_install cvxopt
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Requirement already satisfied: cvxopt in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (1.3.2)
++ pip_install dill
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade dill
Requirement already satisfied: dill in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (0.3.8)
++ pip_install packaging
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (24.1)
++ pip_install matplotlib
++ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Requirement already satisfied: matplotlib in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (3.9.0)
Collecting matplotlib
Using cached matplotlib-3.9.1-cp311-cp311-macosx_11_0_arm64.whl.metadata (11 kB)
Requirement already satisfied: contourpy>=1.0.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (1.2.1)
Requirement already satisfied: cycler>=0.10 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (0.12.1)
Requirement already satisfied: fonttools>=4.22.0 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (4.53.0)
Requirement already satisfied: kiwisolver>=1.3.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (1.4.5)
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 /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (24.1)
Requirement already satisfied: pillow>=8 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (10.3.0)
Requirement already satisfied: pyparsing>=2.3.1 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (3.1.2)
Requirement already satisfied: python-dateutil>=2.7 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from matplotlib) (2.9.0.post0)
Requirement already satisfied: six>=1.5 in /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages (from python-dateutil>=2.7->matplotlib) (1.16.0)
Using cached matplotlib-3.9.1-cp311-cp311-macosx_11_0_arm64.whl (7.8 MB)
Installing collected packages: matplotlib
Attempting uninstall: matplotlib
Found existing installation: matplotlib 3.9.0
Not uninstalling matplotlib at /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages, outside environment /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/venv
Can't uninstall 'matplotlib'. No files were found to uninstall.
Successfully installed matplotlib-3.9.1
++ [[ /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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/src
++ make
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64
cp -p ../include/DARWIN_ARM64 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/DARWIN_ARM64
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make
cp -p ../include/STANALYZER.make /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/STANALYZER.make
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h
cp -p ../include/egads.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h
cp -p ../include/egads_dot.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads_dot.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc
cp -p ../include/egads.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egads.inc
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h
cp -p ../include/egadsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsErrors.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h
cp -p ../include/egadsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h
cp -p ../include/emp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/emp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h
cp -p ../include/prm.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/prm.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h
cp -p ../include/wsserver.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc
cp -p ../include/wsserver.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsserver.inc
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h
cp -p ../include/wsss.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/wsss.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h
cp -p egadsTris.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTris.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h
cp -p egadsSplineFit.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineFit.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h
cp -p egadsSplineVels.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsSplineVels.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc
cp -p ../include/egadsf90.inc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsf90.inc
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealD.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealD_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealD_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealD_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealS.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealS_Lazy.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Lazy.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/SurrealS_Trad.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/SurrealS_Trad.h
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal
cp Surreal/always_inline.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/Surreal/always_inline.h
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsCopy.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsIO.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSplineFit.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSkinning.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessSens.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BRepLib_FuseEdges.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessInp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTris.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsFit.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsRobust.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSBO.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmCfit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmCfit.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmGrid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmGrid.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/prmUV.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsExport.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsEffect.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSolids.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include ../util/emp.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/emp.o
clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaluate.o
clang++ -g -target arm64-apple-darwin -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rational.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/regQuads.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD1
SurrealD1_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealD4
SurrealD4_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS1
SurrealS1_test_suite Complete!
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SurrealS4
SurrealS4_test_suite Complete!
/Library/Developer/CommandLineTools/usr/bin/make -C ../util
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapFindUV.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapGen.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapStructFree.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmapTest.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Read.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_uvmap_Write.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_add.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_add.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_bnd_adj.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_area_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_chk_edge_ratio.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_cpu_message.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_find_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_from_egads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_gen_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibeibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfibf.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_ibfin.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_iccin.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_idibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inibe.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_inl_uv_bnd.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_malloc.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_mben_disc.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_message.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_message.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_norm_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_read.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_solve.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_struct_tasks.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_test.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_to_egads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_version.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. uvmap/uvmap_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap_write.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 egadsUVmap.c -Iuvmap \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsUVmap.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmapStructFree.o EG_uvmapTest.o EG_uvmap_Read.o EG_uvmap_Write.o uvmap_add.o uvmap_bnd_adj.o uvmap_chk_area_uv.o uvmap_chk_edge_ratio.o uvmap_cpu_message.o uvmap_find_uv.o uvmap_from_egads.o uvmap_gen.o uvmap_gen_uv.o uvmap_ibeibe.o uvmap_ibfibf.o uvmap_ibfin.o uvmap_iccibe.o uvmap_iccin.o uvmap_idibe.o uvmap_inibe.o uvmap_inl_uv_bnd.o uvmap_malloc.o uvmap_mben_disc.o uvmap_message.o uvmap_norm_uv.o uvmap_read.o uvmap_solve.o uvmap_struct_tasks.o uvmap_test.o uvmap_to_egads.o uvmap_version.o uvmap_write.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/uvmap.exe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/uvmap.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -luvmap -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegads.dylib egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o \
egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o emp.o evaluate.o rational.o regQuads.o \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a
cp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libuvmap.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; \
ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadstatic.a egadsBase.o egadsMemory.o egadsAttrs.o egadsTess.o egadsTessInp.o egadsTris.o egadsQuads.o egadsFit.o egadsRobust.o egadsSBO.o prmCfit.o prmGrid.o prmUV.o egadsExport.o egadsEffect.o egadsSolids.o egadsGeom.o egadsHLevel.o egadsTopo.o egadsCopy.o egadsSpline.o egadsIO.o egadsSplineFit.o egadsSkinning.o egadsTessSens.o BRepLib_FuseEdges.o emp.o \
evaluate.o rational.o regQuads.o; )
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsHLevel.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsHLevel.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsGeom.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include fgadsTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fgadsTopo.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libfgads.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a emp.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libemp.a
*** EGADS Build Complete! ***
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/wvServer
++ make
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict map.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/map.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include base64-decode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/base64-decode.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/handshake.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include client-handshake.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/client-handshake.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include libwebsockets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libwebsockets.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-deflate-stream.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-deflate-stream.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include md5.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/md5.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension-x-google-mux.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension-x-google-mux.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsers.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsers.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include extension.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extension.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include sha-1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sha-1.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include server.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/server.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include wv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/wv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include browserMessage.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/browserMessage.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fwv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a map.o base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fwv.o; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DLWS_NO_FORK -DSTANDALONE server.c \
-I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/server /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/servertest.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.a \
-lpthread -lz -lm
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang++ -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libwsserver.dylib \
base64-decode.o handshake.o client-handshake.o libwebsockets.o extension-deflate-stream.o md5.o extension-x-google-mux.o parsers.o extension.o sha-1.o server.o wv.o browserMessage.o map.o -lz \
-install_name '@rpath/libwsserver.dylib' \
-compatibility_version 7.8 \
-current_version 1.0.25 )
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/lite
++ make
clang -g -target arm64-apple-darwin -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/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteMemory.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteGeom.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTopo.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteAttrs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteImport.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteString.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTris.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I. -I../src \
../src/egadsQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteTessInp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/evaLite.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE ../util/rational.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ratLite.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I../util \
../util/regQuads.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteRegQuads.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteEffect.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/liteUVmap.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslite.dylib \
liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o liteTess.o liteTris.o liteQuads.o liteTessInp.o \
egadsRobust.o emp.o evaLite.o ratLite.o liteRegQuads.o \
liteEffect.o liteUVmap.o \
-install_name '@rpath/libegadslite.dylib' \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a liteBase.o liteMemory.o liteGeom.o liteTopo.o liteAttrs.o liteImport.o liteString.o \
liteTess.o liteTris.o liteQuads.o liteTessInp.o egadsRobust.o \
emp.o evaLite.o ratLite.o liteRegQuads.o liteEffect.o \
liteUVmap.o ; )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libegadslitestatic.a
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test
+++ ls BSplineIGES.make CSys.make GBO.make SBO.make addKnots.make agglom.make approx.make blend.make chamfer.make closure.make edge2WB.make edges.make effective.make egads2cart.make egads2ply.make egadsGeom_dot.make egadsHLevel_dot.make egadsSpline_dot.make egadsTopo_dot.make exportLite.make extrot.make fillet.make fit.make fitTri.make fullAttr.make fuseSheets.make globalTess.make hollow.make hollowFace.make intersect.make makeCone.make makeFace3D.make makeLoop.make mapTess.make mofb.make mssb.make multiContext.make offset.make rebuild.make refObj.make replace.make revolve.make ruled.make saveTess.make scribe.make sew.make simplePer.make smallEdges.make step.make sweep.make test.make tolerance.make union.make vAttr.make vCurvature.make vEffect.make vEto.make vFrame.make vGeom.make vQuad.make vTess.make vTessInp.make xform.make
++ for file in '`ls *.make`'
++ make -f BSplineIGES.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include BSplineIGES.c -o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/BSplineIGES /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/BSplineIGES.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include CSys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/CSys /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/CSys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include GBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/GBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/GBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include SBO.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/SBO /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/SBO.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include addKnots.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/addKnots /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/addKnots.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include agglom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/agglom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/agglom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include approx.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/approx /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/approx.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \
-legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
++ for file in '`ls *.make`'
++ make -f blend.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include blend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/blend /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/blend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include chamfer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/chamfer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/chamfer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include closure.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/closure /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/closure.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads \
-legads -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
++ for file in '`ls *.make`'
++ make -f edge2WB.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include edge2WB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edge2WB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edge2WB.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include edges.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/edges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/edges.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include effective.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/effective /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/effective.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cart.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cart /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. egads2ply.cpp -std=c++11 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I. tinyply.cpp -std=c++11 -w \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2ply /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2ply.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tinyply.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsGeom_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTools_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsGeom_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsGeom_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsHLevel_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsHLevel_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsHLevel_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsSpline_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsSpline_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsSpline_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egadsTopo_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsTopo_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTopo_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTools_dot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../util/uvmap \
../src/egadsExport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o -DSTANDALONE
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/exportLite /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exportLite.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include extrot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/extrot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/extrot.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fillet.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fillet /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fillet.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fit.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fitTri.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fitTri /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fitTri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fullAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fullAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fullAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fuseSheets.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/fuseSheets /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fuseSheets.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include globalTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/globalTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/globalTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollow /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hollowFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/hollowFace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hollowFace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include intersect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/intersect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/intersect.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeCone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeCone /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeCone.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeFace3D.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeFace3D /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeFace3D.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include makeLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/makeLoop /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/makeLoop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include mapTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mapTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mapTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include mofb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mofb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mofb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include mssb.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/mssb /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mssb.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include multiContext.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/multiContext /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/multiContext.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include offset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/offset /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/offset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include rebuild.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/rebuild /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rebuild.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include refObj.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/refObj /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refObj.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include replace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/replace /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/replace.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include revolve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/revolve /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/revolve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include ruled.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/ruled /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include saveTess.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/saveTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/saveTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include scribe.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/scribe /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/scribe.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include sew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sew /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include simplePer.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/simplePer /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/simplePer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include smallEdges.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/smallEdges /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/smallEdges.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include step.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/step /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/step.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
++ for file in '`ls *.make`'
++ make -f sweep.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include sweep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/sweep /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sweep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include testc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include testf.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testf /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include parsef.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/parsef /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/parsef.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
++ for file in '`ls *.make`'
++ make -f tolerance.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include tolerance.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/tolerance /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tolerance.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/include union.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/union /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/union.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lfgads -legads \
-Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
++ for file in '`ls *.make`'
++ make -f vAttr.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vAttr /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vAttr.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vCurvature.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vCurvature /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vCurvature.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEffect.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEffect /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEffect.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vEto.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vEto /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vEto.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vFrame.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vFrame /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vFrame.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vGeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vGeom /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vGeom.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vQuad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vQuad /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vQuad.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver \
-legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include ../util/retessFaces.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTesstatic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legadstatic -L/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/retessFaces.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vTessInp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vTessInp /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vTessInp.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include xform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/xform /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/EGADS/trunk/docs/Tutorial
++ make -f tire.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include tire.c
clang++ -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
++ make -f egads2tri.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2tri.c
clang++ -g -target arm64-apple-darwin -o egads2tri egads2tri.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/EGADS/trunk/docs/EGADS_dot/src
++ make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle1_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. pingBodies.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o
clang -g -target arm64-apple-darwin -o circle1_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle1_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. circle2_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o
clang -g -target arm64-apple-darwin -o circle2_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/circle2_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o
clang -g -target arm64-apple-darwin -o naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. ruled_naca_dot.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o
clang -g -target arm64-apple-darwin -o ruled_naca_dot /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ruled_naca_dot.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pingBodies.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/src
++ make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. OpenCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. tim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib
clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libocsm.dylib /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/OpenCSM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udp.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lwsserver -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. serveESP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/serveESP /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/serveESP.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. sensCSM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/sensCSM /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sensCSM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBezier.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bezier.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBezier.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBiconvex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/biconvex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBiconvex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/box.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpBspline.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bspline.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpBspline.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCatmull.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/catmull.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCatmull.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCompare.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/compare.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCompare.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreateBEM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createBEM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreateBEM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfCreatePoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/createPoly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfCreatePoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpCsm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/csm.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpCsm.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/deform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDroop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/droop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDroop.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfDumpPmtrs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/dumpPmtrs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfDumpPmtrs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfEditAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/editAttr.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfEditAttr.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEllipse.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ellipse.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEllipse.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpEqn2body.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/eqn2body.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpEqn2body.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFitcurve.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fitcurve.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFitcurve.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfFlend.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flend.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfFlend.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpFreeform.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/freeform.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpFreeform.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGanged.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ganged.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGanged.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfGuide.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/guide.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfGuide.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpHex.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hex.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpHex.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpImport.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/import.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpImport.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpKulfan.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/kulfan.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpKulfan.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfLinalg.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/linalg.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfLinalg.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMatchBodys.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/matchBodys.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMatchBodys.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfMechanism.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mechanism.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfMechanism.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNaca6mc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca6mc.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNaca6mc.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNacelle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nacelle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNacelle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNurbbody.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nurbbody.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNurbbody.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfNuscale.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nuscale.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfNuscale.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfOffset.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/offset.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfOffset.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParabaloid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parabaloid.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParabaloid.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpParsec.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/parsec.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpParsec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPod.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pod.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPod.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpPoly.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/poly.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpPoly.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBbox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBbox.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBbox.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintBrep.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printBrep.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintBrep.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfPrintEgo.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/printEgo.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfPrintEgo.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpProp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/prop.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpProp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpRadwaf.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/radwaf.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpRadwaf.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSample.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sample.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSample.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSew.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sew.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSew.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfShadow.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/shadow.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfShadow.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfSlices.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slices.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfSlices.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpStag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stag.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpStag.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfStiffener.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stiffener.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfStiffener.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpSupell.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/supell.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpSupell.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfTester1.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester1.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfTester1.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpTester2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tester2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpTester2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpVsp3.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vsp3.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpVsp3.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpWaffle.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/waffle.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpWaffle.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udfWarp.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfWarp.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/warp.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udfWarp.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. eggPDT2.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/PDT2.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/eggPDT2.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. udpNaca456.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o
gfortran -g -c -O -frecursive -fcray-pointer naca456.f90 -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -J /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/naca456.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/udpNaca456.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/naca456.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads -lm -static-libgfortran -static-libgcc -Wl,-w
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timEreped.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ereped.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timEreped.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timMitten.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mitten.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timMitten.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlotter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plotter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlotter.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timPlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/plugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timSlugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/slugs.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timSlugs.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timVspSetup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vspSetup.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timVspSetup.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -lwsserver -legads -ldl -lm
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h
cp -p OpenCSM.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/OpenCSM.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h
cp -p common.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/common.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h
cp -p udp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h
cp -p esp.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/esp.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h
cp -p tim.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/tim.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h
cp -p egg.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egg.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h
cp -p udpUtilities.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c
cp -p udpUtilities.c /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/udpUtilities.c
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/docs/UDP_UDF/data
++ make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c -o tire.o
clang -g -target arm64-apple-darwin -o tire tire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DUDP -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include udpTire.c
touch tire.so
rm tire.so
clang -g -target arm64-apple-darwin -bundle -o tire.so udpTire.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib
++ [[ '' == '' ]]
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS
++ make
(cd src; make)
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h
cp -p ../include/caps.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/caps.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h
cp -p ../include/capsErrors.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsErrors.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h
cp -p ../include/capsTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/capsTypes.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h
cp -p ../include/aimUtil.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimUtil.h
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h
cp -p ../include/aimMesh.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aimMesh.h
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \
-I/usr/include/udunits2 aimUtil.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include \
-I/usr/include/udunits2 aimTransferUtil.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../include \
aimMesh.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a
ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimUtil.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimMesh.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtil.o
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libaimUtil.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsBase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBase.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsAnalysis.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAnalysis.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsApprox.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsApprox.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsAttr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAttr.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsBound.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsBound.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsProblem.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsProblem.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsValue.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsValue.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsUnits.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsUnits.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 conjGrad.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/conjGrad.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsFunIDs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsFunIDs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 capsChkInpt.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/capsChkInpt.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. \
-I/usr/include/udunits2 printObject.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/printObject.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; clang -g -target arm64-apple-darwin -dynamiclib -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcaps.dylib capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -ludunits2 -locsm -legads -ldl \
-install_name '@rpath/libcaps.dylib' \
-compatibility_version 1.0.25 \
-current_version 1.0.25 )
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a capsBase.o capsAnalysis.o capsApprox.o capsAttr.o capsAIM.o capsBound.o capsProblem.o capsValue.o capsUnits.o conjGrad.o capsFunIDs.o capsChkInpt.o printObject.o )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libcapsstatic.a
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so
rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include testingWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so
rm: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so: No such file or directory
make[1]: [/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so] Error 1 (ignored)
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/testingWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/testingWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include phaseUtil.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/phaseUtil /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/phaseUtil.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -ludunits2 -locsm -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/attrUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/meshUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cfdUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/feaUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranCards.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/arrayUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/deprecateUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cardUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jsonUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranOP2Reader.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. vlmSpanSpace.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmSpanSpace.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranCards.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libutils.a
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils
cp -p -f arrayUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/aim/utils/vlmUtils.h
/Library/Developer/CommandLineTools/usr/bin/make -C abaqus
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
abaqusAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
abaqusUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/abaqusAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/abaqusFILReader.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -ldl -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C aflr2
clang -g -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr2_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr2c -lm \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_version
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr2AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr2_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr2_Interface.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \
-laflr2c -legen -lrec2 -ldftr2 -ldftr3 -ldgeom -lotb -lqtb -lug_io -lug_cpp -lice2 -lug3 -lug2 -lug_gq -lug -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr3_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr3 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_version
16.32.50
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \
aflr3AIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \
aflr3_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/EG_getEffBodyTopos.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_check_tess_ordering.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_bedge_coord.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_edge_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_faceOrder.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_face_spacing.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_get_surf_grid.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_create_tess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_tess_to_dgeom.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_aflr4_version.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_auto_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ff.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_add_ret_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_bodyFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_check_bc.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_data_cleanup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edgeFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_edit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFace.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceFlag.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceLoop.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_read.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_file_write.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_idef2idef.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_loopEdge.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_nodeData.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_reset_attr.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_setup.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_write_topo_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_curv_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_edge_arclen.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_norm_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_t.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_at_xyz.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_uv_bounds.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_u.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_eval_xyz_at_uv.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_face_node_map.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_cad_geom_faceMatch.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_data.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -D_ENABLE_EGADS_ -w -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src /Users/jenkins/util/AFLR/aflr_lib_11.5.14/src/egads_aflr4/egads_mzone.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr3_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \
-laflr3 -laflr43 -laflr4 -lsurf_auto_cpp -lsurf_auto -lrec3 -lug_mp -lanbl3 -laflr2c -lrec2 -lbl1 -lotb -legen -lice2 -lice3 -ldftr2 -ldftr3 -ldgeom -lug_io -lug_gq -lug_cpp -lcgns -lqtb -lug3 -lug -lug2 -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src aflr4_version.c \
-L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib -laflr4 -lm \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_version
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src -I../utils aflr4AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/AFLR/aflr_lib_11.5.14/src \
-I../utils aflr4_Interface.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/aflr4AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4AIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/EG_getEffBodyTopos.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_check_tess_ordering.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_bedge_coord.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_edge_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_faceOrder.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_face_spacing.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_get_surf_grid.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_create_tess.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_tess_to_dgeom.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_aflr4_version.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_auto_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ff.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_add_ret_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_bodyFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_check_bc.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_data_cleanup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edgeFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_edit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFace.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceFlag.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceLoop.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_read.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_file_write.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_idef2idef.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_loopEdge.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_nodeData.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_reset_attr.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_setup.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_write_topo_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_curv_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_edge_arclen.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_norm_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_t.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_at_xyz.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_uv_bounds.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_u.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_eval_xyz_at_uv.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_face_node_map.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_cad_geom_faceMatch.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_data.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads_mzone.o -L/Users/jenkins/util/AFLR/aflr_lib_11.5.14/MacOSX-arm64/lib \
-laflr4 -laflr2c -lsurf_auto -lsurf_auto_cpp -laflr3 -legen -lrec2 -lrec3 -ldftr3 -ldftr2 -ldgeom -lotb -lqtb -lice2 -lice3 -lug3 -lug2 -lug -lug_mp -lug_gq -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils astrosCards.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/astrosAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/astrosCards.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C avl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils avlAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/avlAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_BODY.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CNC.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_CPOML.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATB.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_DERMATS.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_ELE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_HINGE.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_STRP.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_SURF.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_TOT.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlRead_VM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils awaveAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/awaveAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer -std=legacy awavemod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/awave /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awave.o -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C cart3d
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCAPS_MESHUTILS -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \
cart3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \
-I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D -I./xddm \
writeTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/c3dio \
-I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/libCart3D \
surfTrix.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -pedantic -I./xddm -I. \
`xml2-config --cflags` ./xddm/xddm.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include bodyTess.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cart3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dAIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils \
-laimUtil -locsm -legads -ludunits2 -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ \
-lc3dio -lCart3D -ldl -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include cart3dTest.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/cart3dTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cart3dTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I./xddm \
-I. `xml2-config --cflags` ESPxddm.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/ESPxddm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ESPxddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/writeTrix.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/surfTrix.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xddm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bodyTess.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -locsm -legads \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/ -lc3dio -lCart3D \
-lpthread -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Library/Developer/CommandLineTools/SDKs/MacOSX.sdk/usr/lib -lxml2 -lz -licucore -Wl,-no_compact_unwind -lm
/Library/Developer/CommandLineTools/usr/bin/make -C cbaero
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I. -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o
clang -g -target arm64-apple-darwin -bundle /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cbaeroAIM.o -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/cbaeroAIM.so -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
/Library/Developer/CommandLineTools/usr/bin/make -C cgt
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include egads2cgt.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include aflr4egads.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egads2cgt /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egads2cgt.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aflr4egads.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads -lcaps -locsm -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils delaundoAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/delaundoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/delaundoAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils egadsTessAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/egadsTessAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/egadsTessAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -Wno-format -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils frictionAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/frictionAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -frecursive -fcray-pointer friction_eja_mod.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o
gfortran -g -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/friction /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/friction.o -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C fun3d
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/ugridWriter \
fun3dUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
-I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o
Building FUN3D with Python
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fun3dAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dUtils.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dNamelist.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -lm -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
/Library/Developer/CommandLineTools/usr/bin/make -C hsm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hsmAdj.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict rcm/genrcmi.cpp -DREVISION=7.8 \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/genrcmi.o
/Library/Developer/CommandLineTools/usr/bin/make -C src atanc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/atanc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src bmdump.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bmdump.o
/Library/Developer/CommandLineTools/usr/bin/make -C src cross.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cross.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmabd.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmabd.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbb2.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmbb2.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmbc.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmbc.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmdep.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmdep.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmeqn.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmeqn.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmgeo.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmgeo.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmglr.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmglr.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmout.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmout.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmprj.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmprj.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmre1.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmre1.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmren.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmren.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrfm.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmrfm.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmrun.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmrun.o
/Library/Developer/CommandLineTools/usr/bin/make -C src hsmsol.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmsol.o
/Library/Developer/CommandLineTools/usr/bin/make -C src ludcmp.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ludcmp.o
/Library/Developer/CommandLineTools/usr/bin/make -C src sbsolve.o
gfortran -g -c -O -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sbsolve.o
/Library/Developer/CommandLineTools/usr/bin/make -C src /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a
(cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj; ar -rs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a hsmsol.o hsmdep.o hsmout.o hsmgeo.o hsmabd.o hsmeqn.o hsmbc.o hsmprj.o hsmren.o hsmre1.o hsmrfm.o hsmbb2.o hsmglr.o ludcmp.o sbsolve.o atanc.o bmdump.o cross.o )
ar: creating archive /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libhsm.a
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so
gfortran -g -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/hsmAIM.so \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmAdj.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/rcm.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/genrcmi.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -Wl,-rpath,/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -Wl,-rpath,@loader_path/ -Wl,-rpath,/Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lc++ -static-libgfortran -static-libgcc -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C interference
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. cloudFns.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/interferenceAIM.so \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/cloudFns.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lc++ -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils jfd3AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/jfd3AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/jfd3AIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C masstran
clang++ -g -target arm64-apple-darwin -c -O -fPIC -DOCC_CONVERT_SIGNALS -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-write-strings -Wno-dangling-else -Wno-unused-result -std=c++11 -ffp-model=strict -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils masstranAIM.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/masstranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/masstranAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C meshWriter
/Library/Developer/CommandLineTools/usr/bin/make -C bstlWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include bstlWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bstlWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bstlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bstlWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include bvtkWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bvtkWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/bvtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/bvtkWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C exodusWriter
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -std=c++11 -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include exodusWriter.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exodusWriter.o
clang++ -g -target arm64-apple-darwin -bundle -std=c++11 -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/exodusWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/exodusWriter.o \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C fastWriter
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fastWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/fastWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fastWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include libmeshbWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshbWriter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -IlibMeshb/sources -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include libMeshb/sources/libmeshb7.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/libmeshbWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshbWriter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include stlWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/stlWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/stlWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/stlWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include su2Writer.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2Writer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Writer.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include tecplotWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tecplotWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tecplotWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include ugridWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/ugridWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/ugridWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I../include -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vtkWriter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vtkWriter.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/vtkWriter.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vtkWriter.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -legads -locsm -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils msesUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/msesAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesUtils.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C mystran
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils mystranUtils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/mystranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranUtils.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C nastran
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils nastranAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nastranAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/nastranAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C plato
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include platoAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/platoAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/platoAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/platoAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C pointwise
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils pointwiseAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils hashElement.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pointwiseAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hashElement.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/refineAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSDAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSDAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSDAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSDAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/exodusWriter -I../utils -I/Users/jenkins/util/sandialabs/seacas/include -I/opt/homebrew/include sierraSMAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSMAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSMAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/sierraSMAIM.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils skeletonAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/skeletonAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/skeletonAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include \
-I../meshWriter/exodusWriter \
-I../meshWriter/libmeshbWriter \
-I../utils -I/Users/jenkins/util/sandialabs/seacas/include \
-I/opt/homebrew/include \
spinnakerAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/spinnakerAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/spinnakerAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/spinnakerAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/libmeshb7.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-L/Users/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /Users/jenkins/util/sandialabs/seacas/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C su2
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2Utils.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_4_Cardinal.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_5_Raven.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_6_Falcon.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_7_Blackbird.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils su2_801_Harrier.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_801_Harrier.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/su2AIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2AIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2Utils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_4_Cardinal.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_5_Raven.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_6_Falcon.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_7_Blackbird.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/su2_801_Harrier.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C tacs
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tacsAIM.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tacsAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tacsAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w
/Library/Developer/CommandLineTools/usr/bin/make -C tetgen
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils tetgenAIM.cpp \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I/Users/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
-DTETLIBRARY tetgen_Interface.cpp -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DTETLIBRARY -w /Users/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o
clang++ -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -O0 -w /Users/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tetgenAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgenAIM.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen_Interface.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tetgen.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/predicates.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
tsfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/tsfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/tsfoilAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C unitTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS
cp -p -f pyCAPS/Mesh_Formats.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/Mesh_Formats.py
cp -p -f pyCAPS/test_aflr2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr2.py
cp -p -f pyCAPS/test_aflr3.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr3.py
cp -p -f pyCAPS/test_aflr4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_aflr4.py
cp -p -f pyCAPS/test_astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_astros.py
cp -p -f pyCAPS/test_avl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_avl.py
cp -p -f pyCAPS/test_cart3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cart3d.py
cp -p -f pyCAPS/test_cbaero.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_cbaero.py
cp -p -f pyCAPS/test_egadsTess.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_egadsTess.py
cp -p -f pyCAPS/test_fun3d.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_fun3d.py
cp -p -f pyCAPS/test_masstran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_masstran.py
cp -p -f pyCAPS/test_mses.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_mses.py
cp -p -f pyCAPS/test_pointwise.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_pointwise.py
cp -p -f pyCAPS/test_refine.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_refine.py
cp -p -f pyCAPS/test_su2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_su2.py
cp -p -f pyCAPS/test_tacs.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tacs.py
cp -p -f pyCAPS/test_tetgen.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_tetgen.py
cp -p -f pyCAPS/test_xfoil.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_xfoil.py
cp -p -f pyCAPS/test_zaero.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/test_zaero.py
cp -p -f pyCAPS/Makefile /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/pyCAPS/Makefile
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/airfoilSection.csm
cp -p -f csmData/avlSections.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/avlSections.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfd2D.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSingleBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cfdSingleBody.csm
cp -p -f csmData/cornerGeom.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/cornerGeom.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaSimplePlate.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaWingBEMAero.csm
cp -p -f csmData/feaWingOMLAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/feaWingOMLAero.csm
cp -p -f csmData/kulfanSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSection.csm
cp -p -f csmData/kulfanSymmetricSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/kulfanSymmetricSection.csm
cp -p -f csmData/masstran.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/masstran.csm
cp -p -f csmData/multiRegions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/multiRegions.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/csmData/regions.csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/aimUnitTest/cCAPS
/Library/Developer/CommandLineTools/usr/bin/make -C xfoil
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils \
xfoilAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/xfoilAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/xfoilAIM.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
/Library/Developer/CommandLineTools/usr/bin/make -C zaero
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroAIM.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroAIM.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroUtils.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroUtils.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroLinearFlutter.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroLinearFlutter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroTrim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTrim.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroTypes.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTypes.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroCards.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroCards.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroGeneral.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGeneral.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../utils zaeroGraphical.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGraphical.o
clang -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/zaeroAIM.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroAIM.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroUtils.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroLinearFlutter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTrim.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroTypes.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroCards.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGeneral.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/zaeroGraphical.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
(cd Slugs/src; make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Slugs.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Fitter.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. RedBlackTree.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. Tessellate.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/Slugs /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Slugs.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/RedBlackTree.o \
/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Tessellate.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -legads \
-lpthread -lz -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. TestFit.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/bin/TestFit /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/TestFit.o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/Fitter.o -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -legads \
-lpthread -lz -lm
(cd test; make -f aim.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include aim.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aim.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/test/testingAIM.csm
(cd test; make -f autoExec.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include autoExec.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/autoExec.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm \
-legads -lwsserver -lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include newPhase.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/newPhase /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/newPhase.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib \
-lcaps -locsm -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(cd test; make -f basic.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include basic.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/basic /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/basic.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(cd test; make -f geomIn.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include geomIn.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/geomIn /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/geomIn.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads\
-rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(cd test; make -f utilsTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include aimTransferUtilTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aimTransferUtilTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils miscUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/miscUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -ludunits2 -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I../aim/utils vlmUtilsTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vlmUtilsTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lutils -laimUtil -locsm -legads \
-lpthread -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include vVS.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o
clang++ -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vVS /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/vVS.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lwsserver -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite
cp -p -f pyCAPS/abaqus_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_AGARD445_PyTest.py
cp -p -f pyCAPS/abaqus_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/abaqus_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Astros.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticModal_Fun3D_and_Nastran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Displacement_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Cart3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Pressure_SU2_and_Mystran.py
cp -p -f pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelasticSimple_Temperature_SU2_and_TACS.py
cp -p -f pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_Fun3D_and_Mystran.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Astros.py
cp -p -f pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aeroelastic_Iterative_SU2_and_Mystran.py
cp -p -f pyCAPS/aflr2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr2_PyTest.py
cp -p -f pyCAPS/aflr4_Generic_Missile.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Generic_Missile.py
cp -p -f pyCAPS/aflr4_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_PyTest.py
cp -p -f pyCAPS/aflr4_QuadMesh_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_QuadMesh_PyTest.py
cp -p -f pyCAPS/aflr4_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_TipTreat_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_TipTreat_PyTest.py
cp -p -f pyCAPS/aflr4_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_Tetgen_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_PyTest.py
cp -p -f pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_and_aflr3_Symmetry_PyTest.py
cp -p -f pyCAPS/aflr4_tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/aflr4_tetgen_Regions_PyTest.py
cp -p -f pyCAPS/astros_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_AGARD445_PyTest.py
cp -p -f pyCAPS/astros_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Aeroelastic_PyTest.py
cp -p -f pyCAPS/astros_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/astros_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Composite_PyTest.py
cp -p -f pyCAPS/astros_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Flutter_15degree.py
cp -p -f pyCAPS/astros_MultipleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_MultipleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_OptControl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_OptControl_PyTest.py
cp -p -f pyCAPS/astros_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_PyTest.py
cp -p -f pyCAPS/astros_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/astros_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/astros_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_ThreeBar_PyTest.py
cp -p -f pyCAPS/astros_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/astros_Trim_15degree.py
cp -p -f pyCAPS/autoLink_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/autoLink_Pytest.py
cp -p -f pyCAPS/avl_AutoSpan_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_AutoSpan_PyTest.py
cp -p -f pyCAPS/avl_ControlSurf_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_ControlSurf_PyTest.py
cp -p -f pyCAPS/avl_DesignSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_DesignSweep_PyTest.py
cp -p -f pyCAPS/avl_EigenValue_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_EigenValue_PyTest.py
cp -p -f pyCAPS/avl_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/avl_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/avl_PyTest.py
cp -p -f pyCAPS/awave_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/awave_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_alpha_PyTest.py
cp -p -f pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_OpenMDAO_3_twist_PyTest.py
cp -p -f pyCAPS/cart3d_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cart3d_PyTest.py
cp -p -f pyCAPS/cbaero_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/cbaero_PyTest.py
cp -p -f pyCAPS/delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/delaundo_PyTest.py
cp -p -f pyCAPS/egadsTess_Box_Quad_Pytest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Box_Quad_Pytest.py
cp -p -f pyCAPS/egadsTess_Nose_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Nose_Quad_PyTest.py
cp -p -f pyCAPS/egadsTess_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_PyTest.py
cp -p -f pyCAPS/egadsTess_Spheres_Quad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/egadsTess_Spheres_Quad_PyTest.py
cp -p -f pyCAPS/friction_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/friction_PyTest.py
cp -p -f pyCAPS/fun3d_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_Morph_PyTest.py
cp -p -f pyCAPS/fun3d_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR2_PyTest.py
cp -p -f pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/fun3d_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Delaundo_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_AlphaSweep_PyTest.py
cp -p -f pyCAPS/fun3d_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_and_Tetgen_PyTest.py
cp -p -f pyCAPS/fun3d_refine_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/fun3d_refine_PyTest.py
cp -p -f pyCAPS/hsm_CantileverPlate_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_CantileverPlate_PyTest.py
cp -p -f pyCAPS/hsm_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/hsm_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/masstran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_AGARD445_PyTest.py
cp -p -f pyCAPS/masstran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/masstran_PyTest.py
cp -p -f pyCAPS/mses_OpenMDAO_3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_OpenMDAO_3_PyTest.py
cp -p -f pyCAPS/mses_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mses_PyTest.py
cp -p -f pyCAPS/mystran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_AGARD445_PyTest.py
cp -p -f pyCAPS/mystran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/mystran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_PyTest.py
cp -p -f pyCAPS/mystran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/mystran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_AGARD445_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_AGARD445_PyTest.py
cp -p -f pyCAPS/nastran_Aeroelastic_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Aeroelastic_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_CompositeWingDesign_PyTest.py
cp -p -f pyCAPS/nastran_CompositeWingFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_CompositeWingFreq_PyTest.py
cp -p -f pyCAPS/nastran_Composite_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Composite_PyTest.py
cp -p -f pyCAPS/nastran_Flutter_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Flutter_15degree.py
cp -p -f pyCAPS/nastran_MultiLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_MultiLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_OptimizationMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_OptimizationMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_PlateMisc_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_PlateMisc_PyTest.py
cp -p -f pyCAPS/nastran_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_PyTest.py
cp -p -f pyCAPS/nastran_SingleLoadCase_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_SingleLoadCase_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarFreq_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarFreq_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarLinkDesign_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBarMultiLoad_PyTest.py
cp -p -f pyCAPS/nastran_ThreeBar_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_ThreeBar_PyTest.py
cp -p -f pyCAPS/nastran_Trim_15degree.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/nastran_Trim_15degree.py
cp -p -f pyCAPS/plato_aflr_airfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_airfoil_PyTest.py
cp -p -f pyCAPS/plato_aflr_airfoil_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_airfoil_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_table_PyTest.py
cp -p -f pyCAPS/plato_aflr_table_morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_table_morph_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_aflr_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_aflr_tetgen_table_PyTest.py
cp -p -f pyCAPS/plato_tetgen_cyli_box_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_tetgen_cyli_box_PyTest.py
cp -p -f pyCAPS/plato_tetgen_table_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/plato_tetgen_table_PyTest.py
cp -p -f pyCAPS/pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/pointwise_PyTest.py
cp -p -f pyCAPS/pointwise_Symmetry_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/pointwise_Symmetry_PyTest.py
cp -p -f pyCAPS/su2_Morph_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_Morph_PyTest.py
cp -p -f pyCAPS/su2_X43a_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_X43a_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR2_NodeDist_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR2_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR2_PyTest.py
cp -p -f pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_AFLR4_AFLR3_PyTest.py
cp -p -f pyCAPS/su2_and_Delaundo_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_Delaundo_PyTest.py
cp -p -f pyCAPS/su2_and_Tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_Tetgen_PyTest.py
cp -p -f pyCAPS/su2_and_pointwise_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/su2_and_pointwise_PyTest.py
cp -p -f pyCAPS/tetgen_Holes_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_Holes_PyTest.py
cp -p -f pyCAPS/tetgen_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_PyTest.py
cp -p -f pyCAPS/tetgen_Regions_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tetgen_Regions_PyTest.py
cp -p -f pyCAPS/tsfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/tsfoil_PyTest.py
cp -p -f pyCAPS/xfoil_PyTest.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/pyCAPS/xfoil_PyTest.py
cp -p -f csmData/15degreeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/15degreeWing.csm
cp -p -f csmData/aeroelasticDataTransfer.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/aeroelasticDataTransfer.csm
cp -p -f csmData/aeroelasticDataTransferSimple.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/aeroelasticDataTransferSimple.csm
cp -p -f csmData/airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/airfoilSection.csm
cp -p -f csmData/avlWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.csm
cp -p -f csmData/avlWingTail.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWingTail.csm
cp -p -f csmData/avlWings.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWings.csm
cp -p -f csmData/awaveWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/awaveWingTailFuselage.csm
cp -p -f csmData/cfd2D.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd2D.csm
cp -p -f csmData/cfd2DArbShape.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd2DArbShape.csm
cp -p -f csmData/cfdMultiBody.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdMultiBody.csm
cp -p -f csmData/cfdSymmetry.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdSymmetry.csm
cp -p -f csmData/cfdX43a.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfdX43a.csm
cp -p -f csmData/cfd_airfoilSection.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cfd_airfoilSection.csm
cp -p -f csmData/compositeWing.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/compositeWing.csm
cp -p -f csmData/cyli_box_shell.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_shell.csm
cp -p -f csmData/cyli_box_solid.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/cyli_box_solid.csm
cp -p -f csmData/feaAGARD445.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaAGARD445.csm
cp -p -f csmData/feaBoxes.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaBoxes.csm
cp -p -f csmData/feaCantileverPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaCantileverPlate.csm
cp -p -f csmData/feaJoinedPlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaJoinedPlate.csm
cp -p -f csmData/feaSimplePlate.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaSimplePlate.csm
cp -p -f csmData/feaThreeBar.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaThreeBar.csm
cp -p -f csmData/feaWingBEM.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEM.csm
cp -p -f csmData/feaWingBEMAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/feaWingBEMAero.csm
cp -p -f csmData/frictionWingTailFuselage.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/frictionWingTailFuselage.csm
cp -p -f csmData/generic_missile.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/generic_missile.csm
cp -p -f csmData/interference.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/interference.csm
cp -p -f csmData/linearAero.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/linearAero.csm
cp -p -f csmData/nosecone1.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/nosecone1.csm
cp -p -f csmData/regions.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/regions.csm
cp -p -f csmData/simpleWingBox.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/simpleWingBox.csm
cp -p -f csmData/spheres.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/spheres.csm
cp -p -f csmData/table.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/table.csm
cp -p -f csmData/tiptreat.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/tiptreat.csm
cp -p -f csmData/avlWing.udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/csmData/avlWing.udc
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran
cp -p -f analysisData/nastran/NastranAeroWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranAeroWingBEM.f06
cp -p -f analysisData/nastran/NastranCompositePlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositePlate.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Design.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositeWing_Design.f06
cp -p -f analysisData/nastran/NastranCompositeWing_Freq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranCompositeWing_Freq.f06
cp -p -f analysisData/nastran/NastranFlutter15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranFlutter15Deg.f06
cp -p -f analysisData/nastran/NastranMiscLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranMiscLoadPlate.f06
cp -p -f analysisData/nastran/NastranModalAGARD445.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranModalAGARD445.f06
cp -p -f analysisData/nastran/NastranMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranOptMultiLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranOptMultiLoadPlate.f06
cp -p -f analysisData/nastran/NastranSingleLoadPlate.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranSingleLoadPlate.f06
cp -p -f analysisData/nastran/NastranThreeBar.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBar.f06
cp -p -f analysisData/nastran/NastranThreeBarDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarDesign.f06
cp -p -f analysisData/nastran/NastranThreeBarFreq.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarFreq.f06
cp -p -f analysisData/nastran/NastranThreeBarLinkDesign.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarLinkDesign.f06
cp -p -f analysisData/nastran/NastranThreeBarMultiLoad.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranThreeBarMultiLoad.f06
cp -p -f analysisData/nastran/NastranTrim15Deg.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranTrim15Deg.f06
cp -p -f analysisData/nastran/NastranWingBEM.f06 /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/analysisData/nastran/NastranWingBEM.f06
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm
mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS
cp -p -f corsairlite/boydBox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/boydBox.py
cp -p -f corsairlite/gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/gp.py
cp -p -f corsairlite/hoburg_blackbox.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_blackbox.py
cp -p -f corsairlite/hoburg_gp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/hoburg_gp.py
cp -p -f corsairlite/qp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/qp.py
cp -p -f corsairlite/sp.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/sp.py
cp -p -f corsairlite/capsPhase/csm/wing1.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing1.csm
cp -p -f corsairlite/capsPhase/csm/wing2.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/csm/wing2.csm
cp -p -f corsairlite/capsPhase/pyCAPS/optTaperAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optTaperAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/optWingAvl.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/optWingAvl.py
cp -p -f corsairlite/capsPhase/pyCAPS/sizeWing.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/capsPhase/pyCAPS/sizeWing.py
cp -p -f corsairlite/multifidelity/csm/naca.csm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/csm/naca.csm
cp -p -f corsairlite/multifidelity/pyCAPS/CMConstraint.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/CMConstraint.py
cp -p -f corsairlite/multifidelity/pyCAPS/Camber.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Camber.py
cp -p -f corsairlite/multifidelity/pyCAPS/FlowTrip.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/FlowTrip.py
cp -p -f corsairlite/multifidelity/pyCAPS/GPSize.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/GPSize.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan2.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan2.py
cp -p -f corsairlite/multifidelity/pyCAPS/Kulfan4.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/Kulfan4.py
cp -p -f corsairlite/multifidelity/pyCAPS/MSES.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/MSES.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelKulfan.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelKulfan.py
cp -p -f corsairlite/multifidelity/pyCAPS/fullModelNACA.py /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/corsairlite/multifidelity/pyCAPS/fullModelNACA.py
cp -p -f regressionTest/execute_CTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_CTestRegression.sh
cp -p -f regressionTest/execute_PyTestRegression.sh /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/regressionTest/execute_PyTestRegression.sh
(make -C cCAPS -f aeroelastic_SU2.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticSimple_Iterative_SU2_and_MystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f avlTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include avlTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/avlTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f awaveTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include awaveTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/awaveTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f frictionTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include frictionTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/frictionTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/frictionTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f fun3d.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dAFLR2Test.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dAFLR2Test /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dAFLR2Test.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include fun3dTetgenTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/fun3dTetgenTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/fun3dTetgenTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include aeroelasticTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/aeroelasticTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/aeroelasticTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f hsm.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmSimplePlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmSimplePlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmSimplePlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmCantileverPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmCantileverPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmCantileverPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include hsmJoinedPlateTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/hsmJoinedPlateTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/hsmJoinedPlateTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f interferenceTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include interferenceTest.c \
-o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/interferenceTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f msesTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include msesTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/msesTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -locsm \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f mystran.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include mystranTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/mystranTest.o \
-L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads -ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -lm -ldl
(make -C cCAPS -f pointwiseTest.make)
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include pointwiseTest.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/pointwiseTest.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -legads \
-ludunits2 -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/CAPS/training/ -name Makefile
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//2023/lectures/Makefile == *\l\e\c\t\u\r\e\s* ]]
++ continue
++ for i in '`find $WORKSPACE/CAPS/training/ -name Makefile`'
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//2023/data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//2023/data/session01
++ make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include template_avl.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o
clang -g -target arm64-apple-darwin -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/template_avl /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/template_avl.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -legads -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/CAPS/training//data/session01/Makefile == *\l\e\c\t\u\r\e\s* ]]
+++ dirname /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//data/session01/Makefile
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/training//data/session01
++ make
make: Nothing to be done for `default'.
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/src
++ make -f serveESP.make
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timCapsMode.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/capsMode.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timCapsMode.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timFlowchart.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/flowchart.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timFlowchart.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. timViewer.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/viewer.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timViewer.o -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -lm
clang -g -target arm64-apple-darwin -c -O -Wall -Wno-dangling-else -Wno-unused-result -DREVISION=7.8 -I/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include -I. -I. -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o
touch /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so
rm /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so
clang++ -g -target arm64-apple-darwin -bundle -o /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/pyscript.so /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/obj/timPyscript.o -L/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -ldl -framework CoreFoundation -Wl,-w -L/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -lcaps -locsm -lwsserver -legads -ldl -rpath /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib -rpath @loader_path/ -rpath /Users/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -Wl,-rpath /Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
++ ln -f -s /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/udc /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64
+++ find /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/OpenCSM/trunk/data/training/ -name Makefile
+ mkdir -p /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/test
+ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/test
+ source /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/JenkinsESP/RunRegression.sh
++ [[ 0 == 1 ]]
++ [[ 0 == 2 ]]
++ [[ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64 == '' ]]
++ [[ CAPS/unit == '' ]]
++ [[ 7.8 == '' ]]
++ [[ ! -d /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/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/DARWIN_ARM64/CAPS ]]
++ export CAPSTARGET=unit
++ CAPSTARGET=unit
++ [[ unit == \u\n\i\t ]]
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test
++ ./runUnitTest.sh
++ tee -a capsUnit.txt
=================================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsGeom_dot
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test/egadslog.txt
real 0m3.048s
user 0m1.553s
sys 0m0.073s
+ status=0
+ set +x
=================================================
EGADS test egadsGeom_dot passed (as expected)
=================================================
=================================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsSpline_dot
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test/egadslog.txt
real 0m29.636s
user 0m20.904s
sys 0m0.161s
+ status=0
+ set +x
=================================================
EGADS test egadsSpline_dot passed (as expected)
=================================================
=================================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsTopo_dot
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test/egadslog.txt
real 0m0.709s
user 0m0.254s
sys 0m0.013s
+ status=0
+ set +x
=================================================
EGADS test egadsTopo_dot passed (as expected)
=================================================
=================================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/egadsHLevel_dot
+ tee -a /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/test/egadslog.txt
real 0m0.768s
user 0m0.339s
sys 0m0.013s
+ status=1
+ set +x
=================================================
EGADS test egadsHLevel_dot failed (as expected)
=================================================
All tests pass!
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/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/DARWIN_ARM64/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 = 728
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 = 751
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/DARWIN_ARM64/EGADS/trunk/pyEGADS/test
++ tee -a capsUnit.txt
++ make
python --version
Python 3.11.9
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 73 tests in 3.021s
OK
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/docs/Tutorial
++ python -u tire.py
++ tee -a capsUnit.txt
EGADS Info: 0 Objects, 0 Reference in Use (of 2791) at Close!
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/julia`
Updating registry at `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/registries/General.toml`
Resolving package versions...
Installed CEnum ─────── v0.5.0
Installed Clang_jll ─── v15.0.7+10
Installed JLLWrappers ─ v1.5.0
Installed Preferences ─ v1.4.3
Installed Clang ─────── v0.18.3
Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/Project.toml`
[40e3b903] + Clang v0.18.3
Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/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 v15.0.7+10
[0dad84c5] + ArgTools v1.1.1
[56f22d72] + Artifacts
[2a0f44e3] + Base64
[ade2ca70] + Dates
[f43a241f] + Downloads v1.6.0
[7b1f6079] + FileWatching
[b77e0a4c] + InteractiveUtils
[b27032c2] + LibCURL v0.6.4
[76f85450] + LibGit2
[8f399da3] + Libdl
[56ddb016] + Logging
[d6f4376e] + Markdown
[ca575930] + NetworkOptions v1.2.0
[44cfe95a] + Pkg v1.10.0
[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 v8.4.0+0
[e37daf67] + LibGit2_jll v1.6.4+0
[29816b5a] + LibSSH2_jll v1.11.0+1
[c8ffd9c3] + MbedTLS_jll v2.28.2+1
[14a3606d] + MozillaCACerts_jll v2023.1.10
[83775a58] + Zlib_jll v1.2.13+1
[8f36deef] + libLLVM_jll v15.0.7+10
[8e850ede] + nghttp2_jll v1.52.0+1
[3f19e933] + p7zip_jll v17.4.0+2
Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading. To see why use `status --outdated -m`
Precompiling project...
✓ Zlib_jll
✓ libLLVM_jll
✓ CEnum
✓ Preferences
✓ JLLWrappers
✓ Clang_jll
✓ Clang
7 dependencies successfully precompiled in 13 seconds
Downloading artifact: GCCBootstrap-aarch64-apple-darwin20.v11.0.0-iains.x86_64-linux-musl.unpacked
ERROR: Data Error : jl_gZGF05IFg7-download
Downloading artifact: GCCBootstrap-aarch64-apple-darwin20.v11.0.0-iains.x86_64-linux-musl.unpacked
[ Info: Parsing headers...
[ Info: Processing header: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/include/egadsTypes.h
[ Info: Processing header: /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/Project.toml`
[bba4f53b] + egads v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egads`
Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/Manifest.toml`
[bba4f53b] + egads v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egads`
Test egads
Testing egads
Status `/private/var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jl_QLTVdi/Project.toml`
[bba4f53b] egads v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/jlEGADS/egads`
[fa267f1f] TOML v1.0.3
[8dfed614] Test
Status `/private/var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jl_QLTVdi/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/DARWIN_ARM64/EGADS/trunk/jlEGADS/egads`
⌅ [0ee61d77] Clang_jll v15.0.7+10
[0dad84c5] ArgTools v1.1.1
[56f22d72] Artifacts
[2a0f44e3] Base64
[ade2ca70] Dates
[f43a241f] Downloads v1.6.0
[7b1f6079] FileWatching
[b77e0a4c] InteractiveUtils
[b27032c2] LibCURL v0.6.4
[76f85450] LibGit2
[8f399da3] Libdl
[56ddb016] Logging
[d6f4376e] Markdown
[ca575930] NetworkOptions v1.2.0
[44cfe95a] Pkg v1.10.0
[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
[8dfed614] Test
[cf7118a7] UUIDs
[4ec0a83e] Unicode
[deac9b47] LibCURL_jll v8.4.0+0
[e37daf67] LibGit2_jll v1.6.4+0
[29816b5a] LibSSH2_jll v1.11.0+1
[c8ffd9c3] MbedTLS_jll v2.28.2+1
[14a3606d] MozillaCACerts_jll v2023.1.10
[83775a58] Zlib_jll v1.2.13+1
[8f36deef] libLLVM_jll v15.0.7+10
[8e850ede] nghttp2_jll v1.52.0+1
[3f19e933] p7zip_jll v17.4.0+2
Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading.
Precompiling project...
✓ libLLVM_jll
✓ Zlib_jll
✓ CEnum
✓ Preferences
✓ JLLWrappers
✓ Clang_jll
✓ Test
✓ Clang
✓ egads
9 dependencies successfully precompiled in 11 seconds
1 dependency had output during precompilation:
┌ egads
│ [ Info: ESP_ROOT_LIB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib
└
Testing Running tests...
[ Info: RUNNING TEST test_NMwireBody
[ Info: RUNNING TEST test_addKnots
[ 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_convertToBSpline
[ 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_mergeBSplineCurves
[ Info: RUNNING TEST test_modifyTess
[ Info: RUNNING TEST test_otherCurve
[ Info: RUNNING TEST test_quadTess
[ Info: RUNNING TEST test_removeNodes
[ Info: RUNNING TEST test_revision
[ Info: ********* EGADS version 1.26 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 | 207 207 21.3s
21.310503 seconds (18.53 M allocations: 1.216 GiB, 3.84% gc time, 90.79% 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/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/Project.toml`
[8839a610] + egadslite v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egadslite`
Updating `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/julia/environments/v1.10/Manifest.toml`
[8839a610] + egadslite v0.1.0 `../../../../../EGADS/trunk/jlEGADS/egadslite`
Test egadslite
Testing egadslite
Status `/private/var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jl_uxpCcX/Project.toml`
[8bb1440f] DelimitedFiles v1.9.1
[8839a610] egadslite v0.1.0 `~/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/EGADS/trunk/jlEGADS/egadslite`
[fa267f1f] TOML v1.0.3
[8dfed614] Test
Status `/private/var/folders/l7/7s0m18td3fxg_w_dxpkj1d600000gp/T/jl_uxpCcX/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/DARWIN_ARM64/EGADS/trunk/jlEGADS/egadslite`
⌅ [0ee61d77] Clang_jll v15.0.7+10
[0dad84c5] ArgTools v1.1.1
[56f22d72] Artifacts
[2a0f44e3] Base64
[ade2ca70] Dates
[f43a241f] Downloads v1.6.0
[7b1f6079] FileWatching
[b77e0a4c] InteractiveUtils
[b27032c2] LibCURL v0.6.4
[76f85450] LibGit2
[8f399da3] Libdl
[56ddb016] Logging
[d6f4376e] Markdown
[a63ad114] Mmap
[ca575930] NetworkOptions v1.2.0
[44cfe95a] Pkg v1.10.0
[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
[8dfed614] Test
[cf7118a7] UUIDs
[4ec0a83e] Unicode
[deac9b47] LibCURL_jll v8.4.0+0
[e37daf67] LibGit2_jll v1.6.4+0
[29816b5a] LibSSH2_jll v1.11.0+1
[c8ffd9c3] MbedTLS_jll v2.28.2+1
[14a3606d] MozillaCACerts_jll v2023.1.10
[83775a58] Zlib_jll v1.2.13+1
[8f36deef] libLLVM_jll v15.0.7+10
[8e850ede] nghttp2_jll v1.52.0+1
[3f19e933] p7zip_jll v17.4.0+2
Info Packages marked with ⌅ have new versions available but compatibility constraints restrict them from upgrading.
Precompiling project...
✓ DelimitedFiles
✓ egadslite
2 dependencies successfully precompiled in 4 seconds. 8 already precompiled.
1 dependency had output during precompilation:
┌ egadslite
│ [ Info: ESP_ROOT_LIB /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib
└
Testing Running tests...
[ Info: ********* EGADSLITE version 1.26 OCC (lite version) *********
Test Summary: | Pass Total Time
Julia egadslite API: unit testing | 41 41 1.3s
1.360614 seconds (1.24 M allocations: 85.989 MiB, 2.45% gc time, 94.35% compilation time)
Testing egadslite tests passed
++ cd /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/nastranAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C plato
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/platoAIM.so' is up to date.
/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/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/refineAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSD
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSDAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C sierraSM
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/sierraSMAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C skeleton
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/skeletonAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C spinnaker
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/lib/spinnakerAIM.so' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C su2
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/test/newPhase' is up to date.
(cd test; make -f basic.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/basic' is up to date.
(cd test; make -f geomIn.make)
make[1]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/avlTest' is up to date.
(make -C cCAPS -f awaveTest.make)
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/awaveTest' is up to date.
(make -C cCAPS -f frictionTest.make)
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/interferenceTest' is up to date.
(make -C cCAPS -f msesTest.make)
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/msesTest' is up to date.
(make -C cCAPS -f mystran.make)
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/mystranTest' is up to date.
(make -C cCAPS -f pointwiseTest.make)
make[2]: `/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/examples/cCAPS/pointwiseTest' is up to date.
/Library/Developer/CommandLineTools/usr/bin/make -C pyCAPS/unitTest test
python --version
Python 3.11.9
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!
...............
----------------------------------------------------------------------
Ran 100 tests in 21.853s
OK
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
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 3.11.9
python -u -m unittest discover
......sAnalysis Info:
Name = UnitTest_fun3dAIM
Intent = None
AnalysisDir = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.26
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/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest_fun3dAIM
Version = 1.26
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/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest7_fun3dAIM
Version = 1.26
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/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest8_fun3dAIM
Version = 1.26
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/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest9_fun3dAIM
Version = 1.26
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/DARWIN_ARM64/CAPS/legacy/unitTest/basicTest/Scratch/UnitTest10_fun3dAIM
Version = 1.26
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
284003000 Odd Degenerate test for side 1: 9!
284003000 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
284003000 Odd Degenerate test for side 1: 9!
1E2491C40 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 8.078s
OK (skipped=3)
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.__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: '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 3.11.9
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.028 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.063 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.004 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 = 0.024 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4120 6016
AFLR2 GG : Nodes, Faces = 5820 9416
AFLR2 GG : Nodes, Faces = 7322 12420
AFLR2 GG : Nodes, Faces = 8613 15002
AFLR2 GG : Nodes, Faces = 9793 17362
AFLR2 GG : Nodes, Faces = 10847 19470
AFLR2 GG : Nodes, Faces = 11828 21432
AFLR2 GG : Nodes, Faces = 12749 23274
AFLR2 GG : Nodes, Faces = 13580 24936
AFLR2 GG : Nodes, Faces = 14355 26486
AFLR2 GG : Nodes, Faces = 15088 27952
AFLR2 GG : Nodes, Faces = 15774 29324
AFLR2 GG : Nodes, Faces = 16420 30616
AFLR2 GG : Nodes, Faces = 17013 31802
AFLR2 GG : Nodes, Faces = 17571 32918
AFLR2 GG : Nodes, Faces = 18089 33954
AFLR2 GG : Nodes, Faces = 18573 34922
AFLR2 GG : Nodes, Faces = 19005 35786
AFLR2 GG : Nodes, Faces = 19413 36602
AFLR2 GG : Nodes, Faces = 19779 37334
AFLR2 GG : Nodes, Faces = 20116 38008
AFLR2 GG : Nodes, Faces = 20443 38662
AFLR2 GG : Nodes, Faces = 20756 39288
AFLR2 GG : Nodes, Faces = 21054 39884
AFLR2 GG : Nodes, Faces = 21344 40464
AFLR2 GG : Nodes, Faces = 21621 41018
AFLR2 GG : Nodes, Faces = 21885 41546
AFLR2 GG : Nodes, Faces = 22137 42050
AFLR2 GG : Nodes, Faces = 22387 42550
AFLR2 GG : Nodes, Faces = 22603 42982
AFLR2 GG : Nodes, Faces = 22772 43320
AFLR2 GG : Nodes, Faces = 22912 43600
AFLR2 GG : Nodes, Faces = 23039 43854
AFLR2 GG : Nodes, Faces = 23142 44060
AFLR2 GG : Nodes, Faces = 23205 44186
AFLR2 GG : Nodes, Faces = 23240 44256
AFLR2 GG : Nodes, Faces = 23257 44290
AFLR2 GG : Nodes, Faces = 23269 44314
AFLR2 GG : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.051 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.071 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.085 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.004 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.021 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2224 2224
AFLR2 GG : Nodes, Faces = 4120 6016
AFLR2 GG : Nodes, Faces = 5820 9416
AFLR2 GG : Nodes, Faces = 7322 12420
AFLR2 GG : Nodes, Faces = 8613 15002
AFLR2 GG : Nodes, Faces = 9793 17362
AFLR2 GG : Nodes, Faces = 10847 19470
AFLR2 GG : Nodes, Faces = 11828 21432
AFLR2 GG : Nodes, Faces = 12749 23274
AFLR2 GG : Nodes, Faces = 13580 24936
AFLR2 GG : Nodes, Faces = 14355 26486
AFLR2 GG : Nodes, Faces = 15088 27952
AFLR2 GG : Nodes, Faces = 15774 29324
AFLR2 GG : Nodes, Faces = 16420 30616
AFLR2 GG : Nodes, Faces = 17013 31802
AFLR2 GG : Nodes, Faces = 17571 32918
AFLR2 GG : Nodes, Faces = 18089 33954
AFLR2 GG : Nodes, Faces = 18573 34922
AFLR2 GG : Nodes, Faces = 19005 35786
AFLR2 GG : Nodes, Faces = 19413 36602
AFLR2 GG : Nodes, Faces = 19779 37334
AFLR2 GG : Nodes, Faces = 20116 38008
AFLR2 GG : Nodes, Faces = 20443 38662
AFLR2 GG : Nodes, Faces = 20756 39288
AFLR2 GG : Nodes, Faces = 21054 39884
AFLR2 GG : Nodes, Faces = 21344 40464
AFLR2 GG : Nodes, Faces = 21621 41018
AFLR2 GG : Nodes, Faces = 21885 41546
AFLR2 GG : Nodes, Faces = 22137 42050
AFLR2 GG : Nodes, Faces = 22387 42550
AFLR2 GG : Nodes, Faces = 22603 42982
AFLR2 GG : Nodes, Faces = 22772 43320
AFLR2 GG : Nodes, Faces = 22912 43600
AFLR2 GG : Nodes, Faces = 23039 43854
AFLR2 GG : Nodes, Faces = 23142 44060
AFLR2 GG : Nodes, Faces = 23205 44186
AFLR2 GG : Nodes, Faces = 23240 44256
AFLR2 GG : Nodes, Faces = 23257 44290
AFLR2 GG : Nodes, Faces = 23269 44314
AFLR2 GG : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.062 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23273 44322
AFLR2 : CPU Time = 0.004 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23273
Number of elements = 46546
Number of tris = 44322
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.027 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GG : Nodes, Faces = 2244 2244
AFLR2 GG : Nodes, Faces = 4285 6326
AFLR2 GG : Nodes, Faces = 6135 10026
AFLR2 GG : Nodes, Faces = 7878 13512
AFLR2 GG : Nodes, Faces = 9485 16726
AFLR2 GG : Nodes, Faces = 10981 19718
AFLR2 GG : Nodes, Faces = 12372 22500
AFLR2 GG : Nodes, Faces = 13686 25128
AFLR2 GG : Nodes, Faces = 14908 27572
AFLR2 GG : Nodes, Faces = 16063 29882
AFLR2 GG : Nodes, Faces = 17170 32096
AFLR2 GG : Nodes, Faces = 18222 34200
AFLR2 GG : Nodes, Faces = 19208 36172
AFLR2 GG : Nodes, Faces = 20165 38086
AFLR2 GG : Nodes, Faces = 21087 39930
AFLR2 GG : Nodes, Faces = 21975 41706
AFLR2 GG : Nodes, Faces = 22803 43362
AFLR2 GG : Nodes, Faces = 23582 44920
AFLR2 GG : Nodes, Faces = 24330 46416
AFLR2 GG : Nodes, Faces = 25041 47838
AFLR2 GG : Nodes, Faces = 25723 49202
AFLR2 GG : Nodes, Faces = 26365 50486
AFLR2 GG : Nodes, Faces = 26993 51742
AFLR2 GG : Nodes, Faces = 27556 52868
AFLR2 GG : Nodes, Faces = 28054 53864
AFLR2 GG : Nodes, Faces = 28487 54730
AFLR2 GG : Nodes, Faces = 28847 55450
AFLR2 GG : Nodes, Faces = 29118 55992
AFLR2 GG : Nodes, Faces = 29355 56466
AFLR2 GG : Nodes, Faces = 29553 56862
AFLR2 GG : Nodes, Faces = 29735 57226
AFLR2 GG : Nodes, Faces = 29878 57512
AFLR2 GG : Nodes, Faces = 29969 57694
AFLR2 GG : Nodes, Faces = 30009 57774
AFLR2 GG : Nodes, Faces = 30018 57792
AFLR2 GG : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.130 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 30019 57794
AFLR2 : CPU Time = 0.006 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 30019
Number of elements = 60038
Number of tris = 57794
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 160 272
AFLR2 GG : Nodes, Faces = 172 296
AFLR2 GG : Nodes, Faces = 182 316
AFLR2 GG : Nodes, Faces = 188 328
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.000 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 = 0.005 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.001 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 exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Block: 'Block1_tri', blk_id 1, num_entries 9066
Sideset: 'Airfoil', set_id 1, num_entries 198
Sideset: 'InFlow', set_id 2, num_entries 24
Sideset: 'OutFlow', set_id 3, num_entries 24
Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus 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 = 0.000 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 = 0.012 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 exodus file ....
Exodus expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Block: 'Block1_tri', blk_id 1, num_entries 386
Block: 'Block2_quad', blk_id 2, num_entries 3690
Sideset: 'Airfoil', set_id 1, num_entries 198
Sideset: 'InFlow', set_id 2, num_entries 24
Sideset: 'OutFlow', set_id 3, num_entries 24
Sideset: 'TunnelWall', set_id 4, num_entries 98
Finished writing Exodus 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.000 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 = 0.006 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 = 0.003 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:62938)
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1198
Number of elements = 6307
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4975
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6226
Number of elements = 34532
Number of triangles = 4438
Number of quadrilatarals = 0
Number of tetrahedrals = 30094
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13688
Number of elements = 76798
Number of triangles = 8142
Number of quadrilatarals = 0
Number of tetrahedrals = 68656
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 41861
Number of elements = 237846
Number of triangles = 19888
Number of quadrilatarals = 0
Number of tetrahedrals = 217958
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4339
Number of elements = 24073
Number of triangles = 3010
Number of quadrilatarals = 0
Number of tetrahedrals = 21063
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 11025
Number of elements = 60915
Number of triangles = 8632
Number of quadrilatarals = 0
Number of tetrahedrals = 52283
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10398
Number of elements = 58234
Number of triangles = 6366
Number of quadrilatarals = 0
Number of tetrahedrals = 51868
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 88735
Number of elements = 498705
Number of triangles = 51808
Number of quadrilatarals = 0
Number of tetrahedrals = 446897
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:62938)
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16607
Number of elements = 94482
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 86556
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2585
Number of elements = 13784
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11026
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3615
Number of elements = 19589
Number of triangles = 3392
Number of quadrilatarals = 0
Number of tetrahedrals = 16197
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5438
Number of elements = 30214
Number of triangles = 3654
Number of quadrilatarals = 0
Number of tetrahedrals = 26560
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4697
Number of elements = 26013
Number of triangles = 3324
Number of quadrilatarals = 0
Number of tetrahedrals = 22689
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5467
Number of elements = 30346
Number of triangles = 3754
Number of quadrilatarals = 0
Number of tetrahedrals = 26592
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2273
Number of elements = 12220
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9998
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2405
Number of elements = 12664
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9998
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3357
Number of elements = 18188
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 15078
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3622
Number of elements = 19080
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 15078
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4425
Number of elements = 24045
Number of triangles = 4000
Number of quadrilatarals = 0
Number of tetrahedrals = 20045
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4822
Number of elements = 25381
Number of triangles = 5336
Number of quadrilatarals = 0
Number of tetrahedrals = 20045
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5483
Number of elements = 29853
Number of triangles = 4890
Number of quadrilatarals = 0
Number of tetrahedrals = 24963
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6012
Number of elements = 31633
Number of triangles = 6670
Number of quadrilatarals = 0
Number of tetrahedrals = 24963
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6555
Number of elements = 35742
Number of triangles = 5780
Number of quadrilatarals = 0
Number of tetrahedrals = 29962
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7216
Number of elements = 37966
Number of triangles = 8004
Number of quadrilatarals = 0
Number of tetrahedrals = 29962
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7634
Number of elements = 41677
Number of triangles = 6670
Number of quadrilatarals = 0
Number of tetrahedrals = 35007
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8427
Number of elements = 44345
Number of triangles = 9338
Number of quadrilatarals = 0
Number of tetrahedrals = 35007
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1211
Number of elements = 6379
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5045
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19879
Number of elements = 110275
Number of triangles = 15558
Number of quadrilatarals = 0
Number of tetrahedrals = 94717
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22822
Number of elements = 120055
Number of triangles = 25338
Number of quadrilatarals = 0
Number of tetrahedrals = 94717
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1212
Number of elements = 6382
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1193
Number of elements = 6282
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1217
Number of elements = 6416
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5080
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1200
Number of elements = 6301
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4967
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1190
Number of elements = 6252
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4918
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1204
Number of elements = 6333
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4999
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1211
Number of elements = 6379
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5045
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1220
Number of elements = 6413
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5077
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1214
Number of elements = 6396
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5060
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1192
Number of elements = 6262
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4930
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1201
Number of elements = 6326
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4994
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1206
Number of elements = 6356
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5022
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1187
Number of elements = 6236
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4904
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1197
Number of elements = 6293
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4959
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1180
Number of elements = 6202
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4870
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1197
Number of elements = 6289
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4957
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1208
Number of elements = 6351
Number of triangles = 1334
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 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1193
Number of elements = 6277
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4945
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1200
Number of elements = 6309
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 4975
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8499
Number of elements = 47040
Number of triangles = 6258
Number of quadrilatarals = 0
Number of tetrahedrals = 40782
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8631
Number of elements = 47484
Number of triangles = 6702
Number of quadrilatarals = 0
Number of tetrahedrals = 40782
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7444
Number of elements = 41254
Number of triangles = 5370
Number of quadrilatarals = 0
Number of tetrahedrals = 35884
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1187
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
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9625
Number of elements = 53328
Number of triangles = 7146
Number of quadrilatarals = 0
Number of tetrahedrals = 46182
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9899
Number of elements = 54216
Number of triangles = 8034
Number of quadrilatarals = 0
Number of tetrahedrals = 46182
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7485
Number of elements = 41497
Number of triangles = 5370
Number of quadrilatarals = 0
Number of tetrahedrals = 36127
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1212
Number of elements = 6385
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5053
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1202
Number of elements = 6334
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5002
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9302
Number of elements = 51451
Number of triangles = 6968
Number of quadrilatarals = 0
Number of tetrahedrals = 44483
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9522
Number of elements = 52179
Number of triangles = 7696
Number of quadrilatarals = 0
Number of tetrahedrals = 44483
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7466
Number of elements = 41416
Number of triangles = 5368
Number of quadrilatarals = 0
Number of tetrahedrals = 36048
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1187
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 869
Number of elements = 4533
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3537
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8956
Number of elements = 49469
Number of triangles = 6784
Number of quadrilatarals = 0
Number of tetrahedrals = 42685
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9139
Number of elements = 50065
Number of triangles = 7380
Number of quadrilatarals = 0
Number of tetrahedrals = 42685
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7430
Number of elements = 41197
Number of triangles = 5360
Number of quadrilatarals = 0
Number of tetrahedrals = 35837
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1187
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 522
Number of elements = 2638
Number of triangles = 688
Number of quadrilatarals = 0
Number of tetrahedrals = 1950
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8638
Number of elements = 47663
Number of triangles = 6598
Number of quadrilatarals = 0
Number of tetrahedrals = 41065
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8777
Number of elements = 48099
Number of triangles = 7034
Number of quadrilatarals = 0
Number of tetrahedrals = 41065
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7402
Number of elements = 41032
Number of triangles = 5352
Number of quadrilatarals = 0
Number of tetrahedrals = 35680
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 848
Number of elements = 4402
Number of triangles = 994
Number of quadrilatarals = 0
Number of tetrahedrals = 3408
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2665
Number of triangles = 688
Number of quadrilatarals = 0
Number of tetrahedrals = 1977
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9771
Number of elements = 54406
Number of triangles = 6748
Number of quadrilatarals = 0
Number of tetrahedrals = 47658
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10261
Number of elements = 56170
Number of triangles = 8512
Number of quadrilatarals = 0
Number of tetrahedrals = 47658
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7355
Number of elements = 40784
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 35450
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2663
Number of elements = 14238
Number of triangles = 2794
Number of quadrilatarals = 0
Number of tetrahedrals = 11444
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 243
Number of elements = 1148
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 764
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1510
Number of elements = 7821
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5835
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1574
Number of elements = 7945
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5835
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1170
Number of elements = 6155
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4847
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1630
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 912
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 160
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 76
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5096
Number of elements = 27903
Number of triangles = 4076
Number of quadrilatarals = 0
Number of tetrahedrals = 23827
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5242
Number of elements = 28455
Number of triangles = 4628
Number of quadrilatarals = 0
Number of tetrahedrals = 23827
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4905
Number of elements = 26939
Number of triangles = 4044
Number of quadrilatarals = 0
Number of tetrahedrals = 22895
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 337
Number of elements = 1516
Number of triangles = 584
Number of quadrilatarals = 0
Number of tetrahedrals = 932
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 33115
Number of elements = 191815
Number of triangles = 8476
Number of quadrilatarals = 0
Number of tetrahedrals = 183339
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36459
Number of elements = 205159
Number of triangles = 21820
Number of quadrilatarals = 0
Number of tetrahedrals = 183339
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28820
Number of elements = 163772
Number of triangles = 15148
Number of quadrilatarals = 0
Number of tetrahedrals = 148624
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1416
Number of elements = 7524
Number of triangles = 1456
Number of quadrilatarals = 0
Number of tetrahedrals = 6068
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4240
Number of elements = 23511
Number of triangles = 2950
Number of quadrilatarals = 0
Number of tetrahedrals = 20561
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 720
Number of elements = 3724
Number of triangles = 842
Number of quadrilatarals = 0
Number of tetrahedrals = 2882
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1263
Number of elements = 6628
Number of triangles = 1424
Number of quadrilatarals = 0
Number of tetrahedrals = 5204
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16667
Number of elements = 94472
Number of triangles = 8798
Number of quadrilatarals = 0
Number of tetrahedrals = 85674
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18591
Number of elements = 101848
Number of triangles = 16174
Number of quadrilatarals = 0
Number of tetrahedrals = 85674
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12023
Number of elements = 67478
Number of triangles = 7138
Number of quadrilatarals = 0
Number of tetrahedrals = 60340
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6568
Number of elements = 34370
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25334
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2838
Number of elements = 12404
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 6952
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 6952
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 5440
Finished writing Exodus 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2494
Number of elements = 10977
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6425
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 6425
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 4540
Finished writing Exodus 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) ... ok
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4972
Number of elements = 27531
Number of triangles = 3460
Number of quadrilatarals = 0
Number of tetrahedrals = 24071
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6395
Number of elements = 35692
Number of triangles = 4048
Number of quadrilatarals = 0
Number of tetrahedrals = 31644
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60123
Number of elements = 350900
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 337972
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59547
Number of elements = 346940
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 334512
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60123
Number of elements = 350400
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 337972
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:62938)
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:62938)
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:62938)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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:62938)
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:62938)
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:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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:62938)
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:62938)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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:62938)
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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 1332
Block: 'Wing1_tri', blk_id 2, num_entries 73442
Sideset: 'Farfield', set_id 1, num_entries 1332
Sideset: 'Wing1', set_id 2, num_entries 73442
Finished writing Exodus 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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 300
Block: 'Wing1_tri', blk_id 2, num_entries 32990
Sideset: 'Farfield', set_id 1, num_entries 300
Sideset: 'Wing1', set_id 2, num_entries 32990
Finished writing Exodus 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_regions (test_aflr4.TestAFLR4.test_regions) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = cut, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing exodus file ....
Block: 'box_tri', blk_id 1, num_entries 9130
Block: 'cut_tri', blk_id 2, num_entries 1288
Sideset: 'box', set_id 1, num_entries 9130
Sideset: 'cut', set_id 2, num_entries 1288
Finished writing Exodus 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) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
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_structures (test_aflr4.TestAFLR4.test_structures) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 5
Name = Ribs, index = 1
Name = Skin, index = 2
Name = Spar1, index = 3
Name = Rib_Root, index = 4
Name = Spar2, index = 5
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 2
Name = LeadingEdge, index = 1
Name = TrailingEdge, index = 2
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Ribs
2: Skin
3: Spar1
4: Rib_Root
5: Spar2
Finished writing vtk file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing exodus file ....
Block: 'Ribs_tri', blk_id 1, num_entries 722
Block: 'Skin_tri', blk_id 2, num_entries 16906
Block: 'Spar1_tri', blk_id 3, num_entries 422
Block: 'Rib_Root_tri', blk_id 4, num_entries 292
Block: 'Spar2_tri', blk_id 5, num_entries 166
Sideset: 'Rib_Root', set_id 1, num_entries 292
Sideset: 'Ribs', set_id 2, num_entries 722
Sideset: 'Skin', set_id 3, num_entries 16906
Sideset: 'Spar1', set_id 4, num_entries 422
Sideset: 'Spar2', set_id 5, num_entries 166
Sideset: 'Skin_Top', set_id 6, num_entries 8553
Finished writing Exodus 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_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
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
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
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
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) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 28.284271 -nDiv 9 -maxR 7 -mesh2d > autoInputs.out
Executing: ./aero.csh > aero.out
ok
test_outputs (test_cart3d.TestCart3D.test_outputs) ... ok
test_reenter (test_cart3d.TestCart3D.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD functional.......
Number of design variables - 1
Objective name - Drag
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
Executing: ./aero.csh > aero.out
Executing: ./aero.csh > aero.out
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.307131 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
Executing: ./aero.csh > aero.out
ok
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Mach
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 3
Objective name - C_A
Objective name - C_N
Objective name - C_Y
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:13) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:17) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:18) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:25) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:37:25) Linearizing cut-cells
(22:37:25) ... done
o Number of simultaneous xsensit jobs: 1
(22:37:26) Computing gradients
(22:37:34) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:38) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 3
Objective name - C_D
Objective name - C_L
Objective name - C_S
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:39) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:41) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:43) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:47) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:37:47) Linearizing cut-cells
(22:37:47) ... done
o Number of simultaneous xsensit jobs: 1
(22:37:47) Computing gradients
(22:37:55) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:37:56) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:37:59) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_l
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:00) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:02) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:04) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:06) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:38:06) Linearizing cut-cells
(22:38:06) ... done
o Number of simultaneous xsensit jobs: 1
(22:38:06) Computing gradients
(22:38:10) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:12) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:14) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_m
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:16) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:19) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:20) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:22) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:38:22) Linearizing cut-cells
(22:38:22) ... done
o Number of simultaneous xsensit jobs: 1
(22:38:23) Computing gradients
(22:38:27) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:28) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:30) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_n
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:31) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:35) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:36) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:38) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:38:39) Linearizing cut-cells
(22:38:39) ... done
o Number of simultaneous xsensit jobs: 1
(22:38:39) Computing gradients
(22:38:43) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:44) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:47) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_x
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:48) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:52) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:38:53) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:38:56) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:38:56) Linearizing cut-cells
(22:38:56) ... done
o Number of simultaneous xsensit jobs: 1
(22:38:56) Computing gradients
(22:39:00) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:05) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_y
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:07) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:09) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:10) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:13) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:39:13) Linearizing cut-cells
(22:39:13) ... done
o Number of simultaneous xsensit jobs: 1
(22:39:13) Computing gradients
(22:39:17) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:19) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:21) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Getting CFD functional.......
Number of design variables - 1
Objective name - C_M_z
Done getting CFD functional
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:22) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:25) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:26) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:30) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 1
o Number of simultaneous cutter jobs: 1
(22:39:30) Linearizing cut-cells
(22:39:30) ... done
o Number of simultaneous xsensit jobs: 1
(22:39:30) Computing gradients
(22:39:34) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:35) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:39) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = Wing1, index = 1
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - Mach
Design Variable name - area
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 3
Objective name - C_A
Objective name - C_N
Objective name - C_Y
Done getting CFD functional
Body size = 15.356535
Tessellating body 1 with MaxEdge = 0.383913 Sag = 0.015357 Angle = 15.000000
Executing: autoInputs -r 80.000000 -nDiv 5 -maxR 7 > autoInputs.out
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:42) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:44) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:39:45) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:39:50) aero.csh done
Max memory allowed: 32 GB
Flow hexes: 8744
Estimated cutter memory: 0.000874 GB / DV
Estimated xsensit memory: 0.016614 GB / DV
Available threads: 2
# DVs: 2
o Number of simultaneous cutter jobs: 2
(22:39:50) Linearizing cut-cells
(22:39:52) ... done
o Number of simultaneous xsensit jobs: 2
(22:39:53) Computing gradients
Adjusted OMP_NUM_THREADS to 1 for xsensit
(22:40:01) ... done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
o Evaluating Cart3D functionals and/or gradients
ATTENTION: using static geometry ../inputs/Components.i.tri
(22:40:02) Running aero.csh on 2 core(s) in M0.5A1B0_DP1
(22:40:05) aero.csh done
o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
ok
test_Output_v5 (test_cbaero.TestCBAERO.test_Output_v5) ... 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_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... 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:62938)
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
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
16FD4B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
16FD4B000 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
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
16FD4B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
16FD4B000 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
16FD4B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
16FD4B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 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
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
16FD4B000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
16FD4B000 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:62938)
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:62938)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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:62938)
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:62938)
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:62938)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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:62938)
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:62938)
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:62938)
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:62938)
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:62938)
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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 48
Block: 'Wing1_tri', blk_id 2, num_entries 19110
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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 exodus file ....
Block: 'Farfield_tri', blk_id 1, num_entries 12
Block: 'Wing1_tri', blk_id 2, num_entries 14282
Sideset: 'Farfield', set_id 1, num_entries 12
Sideset: 'Wing1', set_id 2, num_entries 14282
Finished writing Exodus 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) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_egadsTess.TestEGADS.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_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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.130262
Creating surface mesh ...
Surface mesh seconds: 0.026499
Recovering boundaries...
Boundary recovery seconds: 0.131255
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.039712
Recovering Delaunayness...
Delaunay recovery seconds: 0.055723
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 2.14533
Smoothing vertices...
Mesh smoothing seconds: 1.78133
Improving mesh...
Mesh improvement seconds: 0.049958
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.013151
Total running seconds: 4.37354
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.145331
Creating surface mesh ...
Surface mesh seconds: 0.020624
Recovering boundaries...
Boundary recovery seconds: 0.127983
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.038038
Recovering Delaunayness...
Delaunay recovery seconds: 0.054124
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 1.89593
Smoothing vertices...
Mesh smoothing seconds: 1.65189
Improving mesh...
Mesh improvement seconds: 0.033221
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.006586
Total running seconds: 3.97404
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
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/DARWIN_ARM64/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/DARWIN_ARM64/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/DARWIN_ARM64/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 - 5097, elements - 10182
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 - 5097, elements - 10182
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 - 14248, elements - 28484
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 4048
Number of elements = 8092
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8092
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 = 6217
Combined Number of elements = 12425
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12424
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 = 3908
Number of elements = 7812
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7812
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 = 6077
Combined Number of elements = 12145
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12144
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.000 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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 396
Sideset: 'Airfoil', set_id 1, num_entries 18
Sideset: 'InFlow', set_id 2, num_entries 9
Sideset: 'OutFlow', set_id 3, num_entries 9
Sideset: 'TunnelWall', set_id 4, num_entries 18
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 719
Sideset: 'Airfoil', set_id 1, num_entries 17
Sideset: 'InFlow', set_id 2, num_entries 4
Sideset: 'OutFlow', set_id 3, num_entries 18
Sideset: 'TunnelWall', set_id 4, num_entries 22
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tri', blk_id 1, num_entries 1200
Sideset: 'Airfoil', set_id 1, num_entries 20
Sideset: 'InFlow', set_id 2, num_entries 4
Sideset: 'OutFlow', set_id 3, num_entries 36
Sideset: 'TunnelWall', set_id 4, num_entries 40
Finished writing Exodus 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1579
Number of elements = 8634
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7394
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2600
Number of elements = 13872
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11114
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1039
Number of elements = 5509
Number of triangles = 998
Number of quadrilatarals = 0
Number of tetrahedrals = 4511
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 15766
Number of elements = 90668
Number of triangles = 4632
Number of quadrilatarals = 0
Number of tetrahedrals = 86036
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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 86036
Sideset: 'Farfield', set_id 1, num_entries 36
Sideset: 'Wing1', set_id 2, num_entries 4596
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 98795
Sideset: 'Farfield', set_id 1, num_entries 144
Sideset: 'Wing1', set_id 2, num_entries 4086
Finished writing Exodus 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 exodus file ....
Block: 'Block1_tet', blk_id 1, num_entries 163296
Sideset: 'Farfield', set_id 1, num_entries 576
Sideset: 'Wing1', set_id 2, num_entries 5666
Finished writing Exodus 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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1579
Number of elements = 8634
Number of triangles = 1240
Number of quadrilatarals = 0
Number of tetrahedrals = 7394
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 432
Number of elements = 2132
Number of triangles = 644
Number of quadrilatarals = 0
Number of tetrahedrals = 1488
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 935
Number of elements = 5010
Number of triangles = 758
Number of quadrilatarals = 0
Number of tetrahedrals = 4252
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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 23.3.0 arm64
AFLR3 : Compile Date 02/08/24 @ 04:22PM
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 = 0.016 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 25026
AFLR3 IG : Nodes, Elements = 4984 34312
AFLR3 IG : Nodes, Elements = 6227 43517
AFLR3 IG : Nodes, Elements = 6227 43439
AFLR3 IG : Nodes, Elements = 6227 43476
AFLR3 IG : Nodes, Elements = 6227 43444
AFLR3 IG : Nodes, Elements = 6220 26114
AFLR3 IG : Nodes, Elements = 6220 26132
AFLR3 IG : Nodes, Elements = 6220 21569
AFLR3 IG : Nodes, Elements = 6220 19193
AFLR3 : CPU Time = 0.218 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19193
AFLR3 GG : Nodes, Elements = 9101 28053
AFLR3 GG : Nodes, Elements = 9101 39640
AFLR3 GG : Nodes, Elements = 9101 36690
AFLR3 GG : Nodes, Elements = 9101 35155
AFLR3 GG : Nodes, Elements = 11687 43216
AFLR3 GG : Nodes, Elements = 11687 54497
AFLR3 GG : Nodes, Elements = 11687 51170
AFLR3 GG : Nodes, Elements = 11687 50185
AFLR3 GG : Nodes, Elements = 14519 58970
AFLR3 GG : Nodes, Elements = 14519 71103
AFLR3 GG : Nodes, Elements = 14519 67722
AFLR3 GG : Nodes, Elements = 14519 66894
AFLR3 GG : Nodes, Elements = 17597 76360
AFLR3 GG : Nodes, Elements = 17597 89686
AFLR3 GG : Nodes, Elements = 17597 86040
AFLR3 GG : Nodes, Elements = 17597 85134
AFLR3 GG : Nodes, Elements = 20802 94942
AFLR3 GG : Nodes, Elements = 20802 108532
AFLR3 GG : Nodes, Elements = 20802 104847
AFLR3 GG : Nodes, Elements = 20802 104019
AFLR3 GG : Nodes, Elements = 24174 114290
AFLR3 GG : Nodes, Elements = 24174 128631
AFLR3 GG : Nodes, Elements = 24174 124801
AFLR3 GG : Nodes, Elements = 24174 123982
AFLR3 GG : Nodes, Elements = 27742 134809
AFLR3 GG : Nodes, Elements = 27742 150037
AFLR3 GG : Nodes, Elements = 27742 145948
AFLR3 GG : Nodes, Elements = 27742 145081
AFLR3 GG : Nodes, Elements = 31383 156143
AFLR3 GG : Nodes, Elements = 31383 171588
AFLR3 GG : Nodes, Elements = 31383 167421
AFLR3 GG : Nodes, Elements = 31383 166536
AFLR3 GG : Nodes, Elements = 35115 177837
AFLR3 GG : Nodes, Elements = 35115 193748
AFLR3 GG : Nodes, Elements = 35115 189548
AFLR3 GG : Nodes, Elements = 35115 188723
AFLR3 GG : Nodes, Elements = 38948 200319
AFLR3 GG : Nodes, Elements = 38948 216342
AFLR3 GG : Nodes, Elements = 38948 212298
AFLR3 GG : Nodes, Elements = 38948 211481
AFLR3 GG : Nodes, Elements = 42740 222940
AFLR3 GG : Nodes, Elements = 42740 239184
AFLR3 GG : Nodes, Elements = 42740 234883
AFLR3 GG : Nodes, Elements = 42740 234060
AFLR3 GG : Nodes, Elements = 46416 245151
AFLR3 GG : Nodes, Elements = 46416 260680
AFLR3 GG : Nodes, Elements = 46416 256642
AFLR3 GG : Nodes, Elements = 46416 255866
AFLR3 GG : Nodes, Elements = 50035 266777
AFLR3 GG : Nodes, Elements = 50035 281993
AFLR3 GG : Nodes, Elements = 50035 278055
AFLR3 GG : Nodes, Elements = 50035 277383
AFLR3 GG : Nodes, Elements = 53591 288088
AFLR3 GG : Nodes, Elements = 53591 303095
AFLR3 GG : Nodes, Elements = 53591 299307
AFLR3 GG : Nodes, Elements = 53591 298569
AFLR3 GG : Nodes, Elements = 57005 308827
AFLR3 GG : Nodes, Elements = 57005 323244
AFLR3 GG : Nodes, Elements = 57005 319601
AFLR3 GG : Nodes, Elements = 57005 318957
AFLR3 GG : Nodes, Elements = 60293 328832
AFLR3 GG : Nodes, Elements = 60293 342689
AFLR3 GG : Nodes, Elements = 60293 339197
AFLR3 GG : Nodes, Elements = 60293 338647
AFLR3 GG : Nodes, Elements = 63359 347851
AFLR3 GG : Nodes, Elements = 63359 360783
AFLR3 GG : Nodes, Elements = 63359 357437
AFLR3 GG : Nodes, Elements = 63359 356932
AFLR3 GG : Nodes, Elements = 66259 365641
AFLR3 GG : Nodes, Elements = 66259 377775
AFLR3 GG : Nodes, Elements = 66259 374741
AFLR3 GG : Nodes, Elements = 66259 374315
AFLR3 GG : Nodes, Elements = 68879 382177
AFLR3 GG : Nodes, Elements = 68879 393099
AFLR3 GG : Nodes, Elements = 68879 390371
AFLR3 GG : Nodes, Elements = 68879 390020
AFLR3 GG : Nodes, Elements = 71152 396844
AFLR3 GG : Nodes, Elements = 71152 406357
AFLR3 GG : Nodes, Elements = 71152 403836
AFLR3 GG : Nodes, Elements = 71152 403561
AFLR3 GG : Nodes, Elements = 73068 409315
AFLR3 GG : Nodes, Elements = 73068 417362
AFLR3 GG : Nodes, Elements = 73068 415318
AFLR3 GG : Nodes, Elements = 73068 415069
AFLR3 GG : Nodes, Elements = 74529 419454
AFLR3 GG : Nodes, Elements = 74529 425587
AFLR3 GG : Nodes, Elements = 74529 423928
AFLR3 GG : Nodes, Elements = 74529 423776
AFLR3 GG : Nodes, Elements = 75631 427084
AFLR3 GG : Nodes, Elements = 75631 431714
AFLR3 GG : Nodes, Elements = 75631 430512
AFLR3 GG : Nodes, Elements = 75631 430423
AFLR3 GG : Nodes, Elements = 76419 432787
AFLR3 GG : Nodes, Elements = 76419 436211
AFLR3 GG : Nodes, Elements = 76419 435175
AFLR3 GG : Nodes, Elements = 76419 435106
AFLR3 GG : Nodes, Elements = 76934 436651
AFLR3 GG : Nodes, Elements = 76934 438851
AFLR3 GG : Nodes, Elements = 76934 438238
AFLR3 GG : Nodes, Elements = 76934 438198
AFLR3 GG : Nodes, Elements = 77241 439119
AFLR3 GG : Nodes, Elements = 77241 440474
AFLR3 GG : Nodes, Elements = 77241 440052
AFLR3 GG : Nodes, Elements = 77241 440022
AFLR3 GG : Nodes, Elements = 77416 440547
AFLR3 GG : Nodes, Elements = 77416 441274
AFLR3 GG : Nodes, Elements = 77416 441066
AFLR3 GG : Nodes, Elements = 77416 441056
AFLR3 GG : Nodes, Elements = 77509 441335
AFLR3 GG : Nodes, Elements = 77509 441739
AFLR3 GG : Nodes, Elements = 77509 441625
AFLR3 GG : Nodes, Elements = 77509 441612
AFLR3 GG : Nodes, Elements = 77549 441732
AFLR3 GG : Nodes, Elements = 77549 441904
AFLR3 GG : Nodes, Elements = 77549 441849
AFLR3 GG : Nodes, Elements = 77549 441848
AFLR3 GG : Nodes, Elements = 77559 441878
AFLR3 GG : Nodes, Elements = 77559 441913
AFLR3 GG : Nodes, Elements = 77559 441902
AFLR3 GG : Nodes, Elements = 77564 441917
AFLR3 GG : Nodes, Elements = 77564 441932
AFLR3 GG : Nodes, Elements = 77564 441928
AFLR3 GG : Nodes, Elements = 77565 441931
AFLR3 GG : Nodes, Elements = 77565 441938
AFLR3 GG : Nodes, Elements = 77565 441933
AFLR3 GG : Nodes, Elements = 77595 442023
AFLR3 GG : Nodes, Elements = 77595 442128
AFLR3 GG : Nodes, Elements = 77595 442098
AFLR3 GG : Nodes, Elements = 77595 442094
AFLR3 GG : Nodes, Elements = 77599 442106
AFLR3 GG : Nodes, Elements = 77599 442119
AFLR3 GG : Nodes, Elements = 77599 442116
AFLR3 GG : Nodes, Elements = 77599 442115
AFLR3 GG : Nodes, Elements = 77600 442118
AFLR3 GG : Nodes, Elements = 77600 442125
AFLR3 GG : Nodes, Elements = 77600 442121
AFLR3 : CPU Time = 8.574 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 77600 442121
AFLR3 QI : Nodes, Elements = 76105 433678
AFLR3 QI : Nodes, Elements = 75842 432198
AFLR3 QI : Nodes, Elements = 75829 432123
AFLR3 QI : Nodes, Elements = 75827 432113
AFLR3 QI : Nodes, Elements = 75826 432107
AFLR3 QI : Nodes, Elements = 75826 436049
AFLR3 QI : Nodes, Elements = 75826 431912
AFLR3 QI : Nodes, Elements = 75826 431430
AFLR3 QI : Nodes, Elements = 75826 431831
AFLR3 QI : Nodes, Elements = 75826 431146
AFLR3 QI : Nodes, Elements = 75826 430921
AFLR3 QI : Nodes, Elements = 75826 431306
AFLR3 QI : Nodes, Elements = 75826 430921
AFLR3 QI : Nodes, Elements = 75826 430900
AFLR3 QI : Nodes, Elements = 75826 431192
AFLR3 QI : Nodes, Elements = 75826 430885
AFLR3 QI : Nodes, Elements = 75826 430832
AFLR3 QI : Nodes, Elements = 75826 431117
AFLR3 QI : Nodes, Elements = 75826 430836
AFLR3 QI : Nodes, Elements = 75826 430821
AFLR3 QI : Nodes, Elements = 75831 430843
AFLR3 QI : Nodes, Elements = 75831 431136
AFLR3 QI : Nodes, Elements = 75831 430863
AFLR3 QI : Nodes, Elements = 75831 430845
AFLR3 QI : Nodes, Elements = 75831 431106
AFLR3 QI : Nodes, Elements = 75831 430850
AFLR3 QI : Nodes, Elements = 75831 430821
AFLR3 : CPU Time = 2.454 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 75831 430821
AFLR3 QRG: Nodes, Elements = 75839 430867
AFLR3 QRG: Nodes, Elements = 75842 430887
AFLR3 QRG: Nodes, Elements = 75841 430884
AFLR3 QRG: Nodes, Elements = 75841 430883
AFLR3 QRG: Nodes, Elements = 75848 430923
AFLR3 QRG: Nodes, Elements = 75847 430916
AFLR3 : CPU Time = 0.121 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 430916
UG3 : Min, Max Ang = 1.198 173.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 54
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 430916
UG3 : Min Vol = 6.52e-10
UG3 : Average Vol = 4.92
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 = 430916
UG3 : Min, Max Q = 0.073 1
UG3 : Average Q = 0.892
UG3 : No. Q< 0.1 = 27
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 11.945 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 430916
UG3 : Min, Max Ang = 1.198 173.5
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 54
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 430916
UG3 : Min Vol = 6.52e-10
UG3 : Average Vol = 4.92
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 = 430916
UG3 : Min, Max Q = 0.189 1
UG3 : Average Q = 0.85
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 1.26
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 = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
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) ... ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Wing1
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
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 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 75847
Number of elements = 443344
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 430916
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:62938)
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)
16FD4B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
16FD4B000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 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 = 298
Number of elements = 592
Number of triangle elements = 592
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 = 489
Number of elements = 974
Number of triangle elements = 974
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4197
Total number of elements = 8374
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 - 298, elements - 592
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 - 489, elements - 974
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 - 298, elements - 592
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 - 489, elements - 974
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 - 4197, elements - 8374
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 = 173
Number of elements = 342
Number of triangle elements = 342
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 = 2320
Total number of elements = 4604
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 - 173, elements - 342
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 - 173, elements - 342
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 = 443
Number of elements = 882
Number of triangle elements = 882
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 = 965
Total number of elements = 1926
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 443, elements - 882
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 - 443, elements - 882
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 9583, elements - 19158
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 - 7151, elements - 14294
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 = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9583, elements - 19158
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 exodus file ....
Block: 'region_1_tet', blk_id 1, num_entries 104182
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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 - 9583, elements - 19158
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 exodus file ....
Block: 'region_1_tet', blk_id 1, num_entries 69273
Sideset: 'Farfield', set_id 1, num_entries 48
Sideset: 'Wing1', set_id 2, num_entries 19110
Finished writing Exodus 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, 98963.803823, 69822.813293, 6179.981375, 19723.152208, 370546.335525]
ok
----------------------------------------------------------------------
Ran 146 tests in 888.947s
OK (skipped=10)
/Library/Developer/CommandLineTools/usr/bin/make -C legacy/aim/pyCAPS test
python --version
Python 3.11.9
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.013 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6876 13408
AFLR2 : CPU Time = 0.001 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 = 0.000 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 = 0.010 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 = 0.008 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
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 = 0.000 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 = 0.015 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 = 0.006 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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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= 17164 33598 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= 17055 33380 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= 93 152 0
AFLR4 : Nodes, Trias,Quads= 212 390 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 30717 61422 4310
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 30717 61422
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= 25082 48863 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= 81 130 0
AFLR4 : Nodes, Trias,Quads= 210 388 0
AFLR4 : Generate optimal mesh on surface definition 18
AFLR2 : Nodes, Trias,Quads= 81 130 0
AFLR4 : Nodes, Trias,Quads= 209 386 0
DGEOM : Add surface definitions to composite definition 0
DGEOM : Glue composite surface definition 0
DGEOM : Nodes,Faces,BEdges= 63114 126216 8948
AFLR4 : Proximity BG Surface Grid Generation
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
OVERALL : CPU Time = 2.447 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 = 389
Number of elements = 774
Number of triangle elements = 774
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 63114
Total number of elements = 126216
.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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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= 135 228 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= 135 228 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= 17055 33380 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= 17164 33598 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= 134 226 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= 135 228 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 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= 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 = 1.988 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:62938)
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 arm64
AFLR2 : Compile Date 04/23/24 @ 12:51AM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Darwin 23.4.0 arm64
AFLR4 : Compile Date 04/18/24 @ 03:04PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
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= 91 148 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= 310 542 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 = 0.112 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 1.26
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= 91 148 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= 310 542 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 = 0.025 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 1.26
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= 91 148 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= 310 542 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= 91 148 0
AFLR4 : Nodes, Trias,Quads= 86 138 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= 312 546 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= 316 554 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= 1687 3366 498
OVERALL : CPU Time = 0.081 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 = 1218
Number of elements = 2432
Number of triangle elements = 2432
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1687
Total number of elements = 3366
.
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 1.26
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= 91 148 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= 310 542 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= 91 148 0
AFLR4 : Nodes, Trias,Quads= 86 138 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= 312 546 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= 316 554 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= 1522 3036 476
OVERALL : CPU Time = 0.098 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 = 1218
Number of elements = 2432
Number of triangle elements = 2432
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1522
Total number of elements = 3036
.
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 1.26
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= 91 148 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= 310 542 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= 91 148 0
AFLR4 : Nodes, Trias,Quads= 86 138 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= 312 546 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= 316 554 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
OVERALL : CPU Time = 0.071 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 = 1218
Number of elements = 2432
Number of triangle elements = 2432
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1737
Total number of elements = 3466
.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 1.26
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= 135 228 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= 135 228 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= 17055 33380 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= 17164 33598 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= 134 226 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= 135 228 0
AFLR4 : Nodes, Trias,Quads= 132 222 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 137 232 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= 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 = 2.483 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 1.26
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= 36 50 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= 12266 24524 2204
AFLR4 : Curvature BG Surface Grid Generation
AFLR4 : Nodes, Faces = 12266 24524
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 = 1.187 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 1.26
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= 91 148 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= 310 542 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= 91 148 0
AFLR4 : Nodes, Trias,Quads= 86 138 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= 312 546 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= 316 554 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 428
OVERALL : CPU Time = 0.126 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 = 1218
Number of elements = 2432
Number of triangle elements = 2432
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1590
Total number of elements = 3172
.
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 1.26
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= 91 148 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= 310 542 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= 729 1328 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= 91 148 0
AFLR4 : Nodes, Trias,Quads= 86 138 0
AFLR4 : Generate optimal mesh on surface definition 4
AFLR2 : Nodes, Trias,Quads= 314 550 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= 310 542 0
AFLR4 : Nodes, Trias,Quads= 308 538 0
AFLR4 : Generate optimal mesh on surface definition 7
AFLR2 : Nodes, Trias,Quads= 316 554 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 = 0.093 seconds
Body 1 (of 2)
Number of nodes = 664
Number of elements = 1328
Number of triangle elements = 1328
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 1218
Number of elements = 2432
Number of triangle elements = 2432
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
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
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
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
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 = 9573
Number of elements = 19142
Number of triangle elements = 19142
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 6160
Number of elements = 12316
Number of triangle elements = 12316
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 104
Number of elements = 204
Number of triangle elements = 204
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15837
Total number of elements = 31662
.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 = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
.ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62938)
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)
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
17C003000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
1E2491C40 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
1E2491C40 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 = 873
Number of elements = 1742
Number of triangle elements = 1742
Number of quadrilateral elements = 0
Body 3 (of 8)
Number of nodes = 1315
Number of elements = 2626
Number of triangle elements = 2626
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 = 822
Number of elements = 1640
Number of triangle elements = 1640
Number of quadrilateral elements = 0
Body 6 (of 8)
Number of nodes = 1959
Number of elements = 3918
Number of triangle elements = 3918
Number of quadrilateral elements = 0
Body 7 (of 8)
Number of nodes = 935
Number of elements = 1866
Number of triangle elements = 1866
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 = 83220
Total number of elements = 166416
.
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)
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
1E2491C40 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
17C003000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
17C003000 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 = 1959
Number of elements = 3918
Number of triangle elements = 3918
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 = 75689
Total number of elements = 151374
.
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 = 935
Number of elements = 1866
Number of triangle elements = 1866
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 = 74665
Total number of elements = 149322
.
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 = 1315
Number of elements = 2626
Number of triangle elements = 2626
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 = 75045
Total number of elements = 150082
.
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 = 873
Number of elements = 1742
Number of triangle elements = 1742
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 = 74603
Total number of elements = 149198
.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 = 9583
Number of elements = 19158
Number of triangle elements = 19158
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9583
Total number of elements = 19158
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 = 7151
Number of elements = 14294
Number of triangle elements = 14294
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7151
Total number of elements = 14294
. 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 = 822
Number of elements = 1640
Number of triangle elements = 1640
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 = 74552
Total number of elements = 149096
.
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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.131025
Creating surface mesh ...
Surface mesh seconds: 0.023574
Recovering boundaries...
Boundary recovery seconds: 0.119491
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.036043
Recovering Delaunayness...
Delaunay recovery seconds: 0.067815
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 2.07257
Smoothing vertices...
Mesh smoothing seconds: 1.8981
Improving mesh...
Mesh improvement seconds: 0.041516
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.012094
Total running seconds: 4.40259
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
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/DARWIN_ARM64/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/DARWIN_ARM64/CAPS/legacy/aim/pyCAPS/__main__/Scratch/workDir_fun3dTest5_fun3dAIM/fun3d.nml .....
Traceback (most recent call last):
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages/f90nml/parser.py", line 378, in _readstream
Error: Python error occurred while writing namelist file
self._update_tokens()
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/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/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages/f90nml/__init__.py", line 31, in read
return parser.read(nml_path)
^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/python3.11/site-packages/f90nml/parser.py", line 281, in read
return self._readstream(nml_file, nml_patch)
^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
File "/Users/jenkins/util/ESP/Python/ESP_Python-3.11.9/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/DARWIN_ARM64/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/DARWIN_ARM64/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 = 4048
Number of elements = 6648
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 5204
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 = 7800
Number of elements = 15596
Number of triangle elements = 15596
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5906
Number of elements = 11808
Number of triangle elements = 11808
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 542
Number of elements = 1080
Number of triangle elements = 1080
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14248
Total number of elements = 28484
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 - 14248, elements - 28484
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.12528
Creating surface mesh ...
Surface mesh seconds: 0.022247
Recovering boundaries...
Boundary recovery seconds: 0.131803
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.039968
Recovering Delaunayness...
Delaunay recovery seconds: 0.05256
Refining mesh...
18992 insertions, added 13405 points, 688228 tetrahedra in queue.
6324 insertions, added 2619 points, 589108 tetrahedra in queue.
8430 insertions, added 2014 points, 124223 tetrahedra in queue.
Refinement seconds: 1.9985
Smoothing vertices...
Mesh smoothing seconds: 1.82654
Improving mesh...
Mesh improvement seconds: 0.043658
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.01242
Total running seconds: 4.25331
Statistics:
Input points: 14248
Input facets: 28484
Input segments: 42726
Input holes: 2
Input regions: 0
Mesh points: 33028
Mesh tetrahedra: 159264
Mesh faces: 332770
Mesh faces on exterior boundary: 28484
Mesh faces on input facets: 28484
Mesh edges on input segments: 42726
Steiner points inside domain: 18780
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 73.389s
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 0m0.391s
user 0m0.175s
sys 0m0.009s
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aimTransferUtilTest passed (as expected)
=============================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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 0m0.409s
user 0m0.186s
sys 0m0.008s
+ set +x
+ expectCSuccess /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/miscUtilsTest passed (as expected)
=============================================
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest
vlmUtils Tests passed!
real 0m0.395s
user 0m0.165s
sys 0m0.008s
+ set +x
+ rm -rf aimTest
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/vlmUtilsTest passed (as expected)
=============================================
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm
Root Path = /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/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/DARWIN_ARM64/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 = 2006!
testingAIM/aimDiscr: npts = 1062!
testingAIM/aimDiscr: tname = Interface, instance = 0!
testingAIM/aimDiscr: Tessellation set!
testingAIM/aimDiscr: Body 1/Face 6 matches Interface!
testingAIM/aimDiscr: ntris = 772!
testingAIM/aimDiscr: npts = 433!
testingAIM/aimTransfer name = scalar instance = 0 npts = 433/1!
CAPS Info: Bound 'Interface' Normalized Integrated 'scalar'
Rank 0: src = 6.547926e+01, tgt = 6.547926e+01, diff = 1.969212e-09
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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
2 Bodies, 2 Parameters, 6 GeomIns, 2 GeomOuts, 2 Analyses, 1 Bounds
ParamName has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 2
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 2
value = 0.000000 (null)
Param has type VALUE, subtype PARAMETER with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 3
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 3
value = 99 (null)
num has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 6
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 6
value = 8.000000 (null)
x has type VALUE, subtype GEOMETRYIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 7
hist: (null) -> Initial Phase
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:23 1
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 7
linked to ParamName
pVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 16
value = 34.641525 (null)
cVol has type VALUE, subtype GEOMETRYOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 16
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 16
value = 7.296560 (null)
testingAIM0 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
value = 5.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
value (1x3) =
1: Entry1 -> Value1
2: Entry2 -> Value2
3: Entry3 -> Value3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 8
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 18
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
value (0x0) = NULL with len = 0 ego
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 9
testingAIM/aimCalcOutput instance = 0 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 18
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
value = 42 (null)
testingAIM1 has type ANALYSIS, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
4 AnalysisIns, 3 AnalysisOuts, 1 AnalysisDynOs
1 Bodies, 1 Tessellations
testingAIMin has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 10
value = 6.000000 cm
table has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 12
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 12
value (1x3) =
1: Entry1 -> newValue1
2: Entry2 -> newValue2
3: Entry3 -> newValue3
tessIn has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 18
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 13
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
linked to tessOut
meshFile has type VALUE, subtype ANALYSISIN with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 10
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 10
value (0x0) = NULL with len = 0 meter
testingAIMout has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 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 VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
tessOut has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 11
testingAIM/aimCalcOutput instance = 1 index = 2 tessOut 0!
tessPtr = 6000012c01c0
value = 6000012c01c0 ego
lazy: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
meshFile has type VALUE, subtype ANALYSISOUT with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 11
testingAIM/aimCalcOutput instance = 1 index = 3 meshFile 0!
value (0x0) = NULL with len = 0 writer
lazy: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
Everything has type VALUE, subtype ANALYSISDYNO with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 28
value = 42 (null)
Interface has type BOUND, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 14
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
2 Connecteds, 0 UnConnecteds
testingAIM1 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
5 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
1062 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
1062 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 26
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 15
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:46 26
1062 points, rank=1, units=(null)
testingAIM0 has type VERTEXSET, subtype CONNECTED with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
6 DataSets
xyz has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
433 points, rank=3, units=cm
xyzd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
0 points, rank=3, units=(null)
param has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 23
433 points, rank=2, units=(null)
paramd has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
0 points, rank=2, units=(null)
scalar has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 25
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Child Execute
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 25
433 points, rank=1, units=(null)
vector has type DATASET, subtype NONE with 0 attributes
last: aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
hist: (null) -> Starting
aimTest VIGGEN.MIT.EDU:27833 jenkins 2024/07/11 22:49:24 0
testingAIM/aimTransfer name = vector instance = 0 npts = 433/3!
433 points, rank=3, units=(null)
1: 14.400001 14.400001 14.400000 14.400001 14.400001 14.400000 14.400000
8: 14.400001 14.400000 14.400003 14.380571 14.400001 14.381441 14.400000
15: 14.400000 14.400002 14.400002 14.400000 14.400000 14.400002 14.400000
22: 14.400001 14.400001 14.400000 14.383000 14.400000 14.400000 14.400001
29: 14.400000 14.390397 14.400001 14.400000 14.400000 14.400002 14.400002
36: 14.400001 14.400001 14.390256 14.400001 14.389522 14.400002 14.400002
43: 14.400002 14.400000 14.400000 14.400002 14.400003 14.400003 14.400003
50: 14.400000 14.379777 14.400000 14.400001 14.378056 14.400000 14.400000
57: 14.400000 14.400001 14.376355 14.400002 14.400000 14.400000 14.400001
64: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400000 14.400001
71: 14.381349 14.400000 14.400002 14.400002 14.400002 14.400000 14.400000
78: 14.400000 14.400000 14.400001 14.400001 14.390810 14.400001 14.384482
85: 14.400000 14.400000 14.400001 14.400001 14.400001 14.400001 14.400000
92: 14.400002 14.400000 14.400000 14.400001 14.400001 14.400001 14.400000
99: 14.400000 14.400002 14.400000 14.400002 14.400000 14.400000 14.400000
106: 14.400002 14.400002 14.400002 14.400003 14.400003 14.400003 14.400003
113: 14.400003 14.400000 14.400000 14.400000 14.400001 14.400001 14.400001
120: 14.400002 14.400000 14.399999 14.400001 14.400002 14.400001 14.400002
127: 14.400001 14.400001 14.400000 14.400001 14.400001 14.400001 14.400002
134: 14.400002 14.400002 14.400002 14.400002 14.400003 14.400001 14.400001
141: 14.400002 14.400001 14.400002 14.400001 14.400002 14.400001 14.400002
148: 14.399999 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001
155: 14.400001 14.400001 14.400001 14.400003 14.400001 14.400001 14.400001
162: 14.400001 14.400001 14.400002 14.400001 14.400001 14.400000 14.400001
169: 14.400001 14.400001 14.400001 14.400000 14.400001 14.400001 14.400002
176: 14.400000 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002
183: 14.400001 14.400002 14.400002 14.400001 14.400001 14.400002 14.400001
190: 14.400001 14.400001 14.400002 14.399999 14.400001 14.400002 14.400002
197: 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001 14.400001
204: 14.400002 14.400001 14.400001 14.400002 14.400002 14.400002 14.400002
211: 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001
218: 14.400000 14.400001 14.400002 14.400001 14.400001 14.400002 14.400001
225: 14.400001 14.400001 14.400002 14.400002 14.400002 14.400001 14.400001
232: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400000
239: 14.400000 14.400002 14.400000 14.400001 14.400001 14.400001 14.400002
246: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
253: 14.400002 14.400002 14.400001 14.400001 14.400001 14.400001 14.400001
260: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
267: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001 14.400001
274: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400002
281: 14.400001 14.400001 14.400000 14.400001 14.399999 14.400001 14.400002
288: 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001
295: 14.400003 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001
302: 14.400002 14.400001 14.400001 14.400000 14.400001 14.400002 14.400000
309: 14.400002 14.400001 14.400001 14.400001 14.400002 14.400001 14.400000
316: 14.400001 14.400001 14.400001 14.400002 14.400001 14.400001 14.399999
323: 14.400001 14.400001 14.355208 14.400002 14.400002 14.400001 14.400001
330: 14.400000 14.400000 14.400001 14.399999 14.400001 14.400000 14.400001
337: 14.400001 14.400001 14.400003 14.400002 14.399999 14.400001 14.400000
344: 14.400002 14.400001 14.400002 14.400001 14.400001 14.400001 14.400001
351: 14.400002 14.400001 14.400000 14.400006 14.400002 14.400001 14.400000
358: 14.400000 14.400001 14.400001 14.400001 14.399999 14.400002 14.400001
365: 14.400001 14.400002 14.400000 14.400001 14.357384 14.400000 14.399999
372: 14.400002 14.400002 14.400002 14.400001 14.400001 14.400001 14.399999
379: 14.400001 14.399999 14.400002 14.400002 14.400001 14.400001 14.400001
386: 14.400002 14.400000 14.399999 14.400001 14.400001 14.400000 14.400000
393: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400002 14.400001
400: 14.400002 14.400001 14.399999 14.400002 14.399999 14.400001 14.400001
407: 14.400000 14.400001 14.400002 14.400001 14.400002 14.400001 14.400001
414: 14.400001 14.400001 14.400001 14.400001 14.400001 14.400004 14.359138
421: 14.400005 14.399999 14.400001 14.400000 14.400001 14.400001 14.400001
428: 14.400002 14.399999 14.400000 14.400000 14.400002 14.400001 14.400004
435: 14.400004 14.362514 14.362329 14.400001 14.399999 14.400001 14.400001
442: 14.400001 14.400001 14.400002 14.400003 14.399999 14.400001 14.400002
449: 14.400001 14.400001 14.400002 14.400001 14.399999 14.400001 14.399999
456: 14.400001 14.400002 14.400004 14.400000 14.399999 14.400000 14.400000
463: 14.400001 14.399999 14.362644 14.400001 14.400002 14.399999 14.399999
470: 14.400001 14.400001 14.400001 14.399999 14.400001 14.400001 14.366558
477: 14.400001 14.400006 14.400001 14.400000 14.400001 14.400000 14.400001
484: 14.400004 14.400001 14.400005 14.399999 14.400002 14.400001 14.400005
491: 14.399999 14.400002 14.399999 14.367443 14.400003 14.400001 14.400000
498: 14.400001 14.400001 14.362493 14.399999 14.400001 14.399999 14.400001
505: 14.399999 14.400005 14.399999 14.400004 14.400001 14.400004 14.363391
512: 14.400001 14.366127 14.400002 14.400004 14.399999 14.400001 14.400004
519: 14.399999 14.400001 14.399999 14.400001 14.364370 14.399999 14.400005
526: 14.400005 14.365691 14.399999 14.369927 14.400002 14.400001 14.400000
533: 14.400000 14.368701 14.400001 14.399999 14.400000 14.399999 14.364370
540: 14.360914 14.399999 14.400001 14.400005 14.400004 14.400002 14.399999
547: 14.400000 14.399999 14.366320 14.400001 14.400003 14.370716 14.367841
554: 14.367007 14.367819 14.399999 14.369566 14.400001 14.399999 14.399999
561: 14.366648 14.367456 14.400005 14.400002 14.366344 14.400000 14.369947
568: 14.400004 14.400004 14.367007 14.373369 14.400001 14.400000 14.400002
575: 14.365408 14.400004 14.400000 14.400004 14.399999 14.400005 14.400002
582: 14.399999 14.400002 14.400001 14.400004 14.400004 14.369590 14.400004
589: 14.372211 14.400002 14.400000 14.400002 14.400002 14.400003 14.400000
596: 14.400004 14.400004 14.373403 14.368774 14.400000 14.400000 14.399999
603: 14.400001 14.400002 14.370406 14.367007 14.400001 14.372363 14.400001
610: 14.370598 14.400000 14.399999 14.400002 14.400004 14.372320 14.400000
617: 14.400000 14.368054 14.400004 14.400000 14.378759 14.400000 14.366320
624: 14.400000 14.400000 14.400004 14.370366 14.370760 14.400002 14.400004
631: 14.400004 14.400004 14.369692 14.365169 14.400004 14.400004 14.400000
638: 14.399999 14.400005 14.368369 14.400001 14.400000 14.400000 14.400003
645: 14.400003 14.399999 14.400002 14.400001 14.370996 14.400001 14.400002
652: 14.400002 14.367680 14.400000 14.400004 14.400000 14.400003 14.400003
659: 14.367301 14.400000 14.371052 14.400000 14.400004 14.375426 14.372158
666: 14.400000 14.370146 14.399999 14.400004 14.399999 14.368248 14.400000
673: 14.400003 14.369989 14.370548 14.368054 14.377207 14.400000 14.369613
680: 14.368333 14.400004 14.400001 14.377741 14.400003 14.400000 14.400004
687: 14.400003 14.400003 14.400000 14.377967 14.399999 14.376780 14.370538
694: 14.373367 14.400000 14.400003 14.400004 14.370294 14.371052 14.400000
701: 14.400003 14.370426 14.400004 14.400001 14.400001 14.376281 14.375920
708: 14.377357 14.400000 14.376914 14.400001 14.400002 14.400002 14.400002
715: 14.400003 14.379840 14.370996 14.400003 14.400003 14.370673 14.400000
722: 14.363653 14.362250 14.373534 14.400003 14.379510 14.400000 14.374657
729: 14.400003 14.400004 14.400002 14.379679 14.400000 14.379827 14.372479
736: 14.400002 14.380745 14.379344 14.379423 14.400003 14.380718 14.372490
743: 14.376209 14.400000 14.400000 14.400000 14.400000 14.400000 14.400003
750: 14.375014 14.373465 14.400000 14.400003 14.380638 14.400002 14.400002
757: 14.400000 14.376150 14.400003 14.400003 14.370382 14.379062 14.379044
764: 14.382714 14.371636 14.380688 14.372490 14.400004 14.380301 14.400003
771: 14.400003 14.400003 14.400003 14.381338 14.400003 14.400000 14.375566
778: 14.383460 14.400000 14.400000 14.382573 14.378742 14.378784 14.400002
785: 14.400003 14.377962 14.400003 14.388515 14.372960 14.400003 14.373659
792: 14.400000 14.376226 14.400000 14.400000 14.373627 14.400000 14.400002
799: 14.379592 14.400001 14.384129 14.381281 14.380925 14.400002 14.400000
806: 14.376874 14.400003 14.400000 14.376488 14.400002 14.372785 14.382064
813: 14.400002 14.400002 14.400002 14.400002 14.400002 14.400003 14.400003
820: 14.375490 14.374772 14.400003 14.375179 14.376681 14.379475 14.400003
827: 14.374392 14.379479 14.377005 14.387430 14.400002 14.382223 14.400003
834: 14.374371 14.383997 14.382259 14.386520 14.400000 14.400002 14.384358
841: 14.381380 14.373136 14.380004 14.382103 14.400002 14.400000 14.376043
848: 14.400000 14.381875 14.400002 14.377417 14.379456 14.400000 14.379534
855: 14.400002 14.400003 14.400000 14.400003 14.400000 14.400000 14.382400
862: 14.384944 14.376706 14.383227 14.400002 14.380291 14.400002 14.382257
869: 14.400003 14.384774 14.384820 14.382273 14.373450 14.400000 14.400003
876: 14.375908 14.378550 14.400000 14.377290 14.382472 14.379168 14.383016
883: 14.385491 14.382723 14.400003 14.400002 14.378971 14.385404 14.380466
890: 14.384576 14.400003 14.377221 14.400000 14.381355 14.383645 14.384247
897: 14.385287 14.383280 14.375114 14.400002 14.400000 14.400000 14.400000
904: 14.382426 14.382735 14.400002 14.382499 14.387660 14.382883 14.400002
911: 14.383520 14.387020 14.383842 14.382243 14.400000 14.378098 14.383884
918: 14.383573 14.384907 14.386099 14.400002 14.383499 14.385888 14.400002
925: 14.377060 14.378436 14.381620 14.380706 14.400000 14.373575 14.383742
932: 14.381255 14.382997 14.384659 14.382920 14.400000 14.400002 14.377577
939: 14.400000 14.386915 14.386123 14.384593 14.381816 14.381745 14.385286
946: 14.385286 14.382005 14.385759 14.385133 14.388988 14.381642 14.387570
953: 14.386633 14.386532 14.381505 14.386235 14.385447 14.400000 14.380013
960: 14.400000 14.382953 14.400002 14.383380 14.385229 14.383810 14.382999
967: 14.385309 14.400002 14.400002 14.382711 14.383198 14.385759 14.387667
974: 14.385183 14.384109 14.387476 14.400002 14.384433 14.388306 14.400002
981: 14.400002 14.383798 14.386396 14.386806 14.383774 14.389577 14.400000
988: 14.379854 14.381554 14.377995 14.375728 14.378018 14.382139 14.386343
995: 14.386055 14.378954 14.383869 14.400002 14.383263 14.385113 14.381831
1002: 14.400002 14.386892 14.388833 14.386742 14.385055 14.385000 14.381934
1009: 14.381408 14.380687 14.379175 14.380043 14.381323 14.375969 14.381364
1016: 14.384193 14.380959 14.400002 14.400002 14.400002 14.385962 14.400002
1023: 14.386889 14.381389 14.400002 14.379351 14.387189 14.400000 14.382624
1030: 14.400002 14.387047 14.400002 14.386889 14.379175 14.377388 14.389345
1037: 14.400002 14.400000 14.400000 14.381891 14.380687 14.400002 14.400000
1044: 14.383688 14.400002 14.400002 14.400002 14.383791 14.400000 14.400002
1051: 14.400003 14.400000 14.376605 14.400002 14.400000 14.376130 14.400003
1058: 14.383633 14.400002 14.400000 14.378191 14.384880
source getTriangles = 0, nGtris = 2006, nGsegs = 6018, Ds = 0 0
destin getTriangles = 0, nGtris = 772, nGsegs = 2316, Ds = 0 0
In caps_outputObjects:
2 Analyses found
1 Bounds found
testingAIM/aimCleanup instance = 0!
testingAIM/aimCleanup instance = 1!
real 0m23.358s
user 0m16.433s
sys 0m0.434s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/aim testingAIM.csm passed (as expected)
=============================================
+ rm -rf source.vs destin.vs
+ expectCSuccess '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm'
+ /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/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/DARWIN_ARM64/CAPS/test/autoExecTest/Scratch/testingAIM1
UnitSys = (null)
Exec = 2
Fields = scalar (1 1) vector (3 1) scalar (1 0) vector (3 0)
Dirty = 3
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/DARWIN_ARM64/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!
real 0m1.406s
user 0m0.595s
sys 0m0.160s
+ set +x
=============================================
CAPS test (using c-executables) case /Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64/ESP/DARWIN_ARM64/test/autoExec testingAIM.csm passed (as expected)
=============================================
++ set +x
[Execution node] check if [viggen] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping repository mining
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Clang] Skipping post processing
[Clang] No filter has been set, publishing all 0 issues
[Clang] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/Users/jenkins/workspace/ESP_RegCaps/7.8/CAPS/unit/DARWIN_ARM64')
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] No valid reference build found
[Static Analysis] All reported issues will be considered outstanding
[Static Analysis] No quality gates have been set - skipping
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_RegCaps/CASREV=7.8,ESPTEST=CAPS/unit,ESP_ARCH=DARWIN_ARM64,buildnode=viggen #671'.
[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