Started by upstream project "ESP_Beta" build number 723
originally caused by:
 Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds in workspace /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] Done
Checking out a fresh workspace because there's no workspace at /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-06-18T21:16:10.397 -0400' --quiet
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 2506

Checking out a fresh workspace because /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-06-18T21:16:10.397 -0400' --quiet
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 867

No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP 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 shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64.ifort] $ /bin/bash -ex /tmp/jenkins14283871202324573135.sh
+ bash -ex /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/ESP_Beta.sh
+ source /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds == \r\e\y\n\o\l\d\s ]]
++ [[ LINUX64.ifort == \L\I\N\U\X\6\4\.\g\n\u* ]]
++ [[ LINUX64.ifort == *\.\i\f\o\r\t ]]
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export EFCOMP=ifort
++ EFCOMP=ifort
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ source /opt/intel/oneapi/setvars.sh
++ '[' -f /home/jenkins/.bashrc ']'
++ source /home/jenkins/.bashrc
+++ DEBUG_MODE=0
+++ [[ ehxB == *x* ]]
+++ DEBUG_MODE=1
+++ set +x
+++ case $- in
+++ return
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64
++ ESP_BLOC=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64
++ export ESP_ROOT=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64
++ ESP_ROOT=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds == *\r\e\y\n\o\l\d\s* ]]
++ [[ '' != '' ]]
++ [[ -d /home/jenkins/util/ESP/Python/ESP_Python-3.11.9 ]]
++ export PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ export PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ export EMPnumProc=4
++ EMPnumProc=4
++ export OMP_NUM_THREADS=4
++ OMP_NUM_THREADS=4
++ '[' '!' -z '' ']'
+++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ LD_LIBRARY_PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ export ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ ESP_EXTERN_LIBS=/home/jenkins/util/ESP/ExternLibs
++ export AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ CART3D=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16
++ export CART3D_ARCH=X86_64_ICC
++ CART3D_ARCH=X86_64_ICC
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ MYSTRAN_directory=/home/jenkins/util/mystran/MYSTRAN/Binaries
++ export PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ export CAPS_GLYPH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/aim/pointwise/glyph
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin
++ [[ reynolds == \r\e\y\n\o\l\d\s ]]
++ export SEACAS=/home/jenkins/util/sandialabs/seacas
++ SEACAS=/home/jenkins/util/sandialabs/seacas
++ export SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ SU2_HOME=/home/jenkins/util/SU2/SU2-v8.0.0
++ export SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ SU2_RUN=/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ '[' -d /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16 ']'
+++ perl -I/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5 -Mlocal::lib=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
++ eval 'PATH="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin${PATH:+:${PATH}}"; export PATH;
PERL5LIB="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5${PERL5LIB:+:${PERL5LIB}}"; export PERL5LIB;
PERL_LOCAL_LIB_ROOT="/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl${PERL_LOCAL_LIB_ROOT:+:${PERL_LOCAL_LIB_ROOT}}"; export PERL_LOCAL_LIB_ROOT;
PERL_MB_OPT="--install_base \"/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl\""; export PERL_MB_OPT;
PERL_MM_OPT="INSTALL_BASE=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl"; export PERL_MM_OPT;'
+++ PATH=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
+++ export PATH
+++ PERL5LIB=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/lib/perl5
+++ export PERL5LIB
+++ PERL_LOCAL_LIB_ROOT=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
+++ export PERL_LOCAL_LIB_ROOT
+++ PERL_MB_OPT='--install_base "/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl"'
+++ export PERL_MB_OPT
+++ PERL_MM_OPT=INSTALL_BASE=/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl
+++ export PERL_MM_OPT
++ export PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/pyCAPS:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/pyCAPS:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds == \m\a\c\y\s* ]]
++ [[ reynolds == \v\i\g\g\e\n ]]
+++ python-config --includes
++ export 'PYTHONINC=. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
++ PYTHONINC='. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11'
+++ python-config --help
++ [[ Usage: /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/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/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl  -lutil -lm '
++ PYTHONLIB=' -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lpthread -ldl  -lutil -lm '
++ [[ reynolds == \m\a\c\y\s ]]
++ [[ reynolds == \v\i\g\g\e\n ]]
++ export PYTHONUNBUFFERED=true
++ PYTHONUNBUFFERED=true
++ export PYTHONFAULTHANDLER=true
++ PYTHONFAULTHANDLER=true
++ python --version
Python 3.11.9
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export CSMDATA=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/data
++ CSMDATA=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/data
+ virtualenv /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 147ms
  creator CPython3Posix(dest=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv, clear=False, no_vcs_ignore=False, global=False)
  seeder FromAppData(download=False, pip=bundle, setuptools=bundle, wheel=bundle, via=copy, app_data_dir=/home/jenkins/.local/share/virtualenv)
    added seed packages: pip==24.0, setuptools==70.0.0, wheel==0.43.0
  activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/activate
++ '[' /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/activate = /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/ESP_Beta.sh ']'
++ deactivate nondestructive
++ unset -f pydoc
++ '[' -z '' ']'
++ '[' -z '' ']'
++ hash -r
++ '[' -z '' ']'
++ unset VIRTUAL_ENV
++ unset VIRTUAL_ENV_PROMPT
++ '[' '!' nondestructive = nondestructive ']'
++ VIRTUAL_ENV=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv
++ VIRTUAL_ENV_PROMPT=ESP_venv
++ export VIRTUAL_ENV_PROMPT
++ '[' -z _ ']'
++ _OLD_VIRTUAL_PYTHONHOME=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9
++ unset PYTHONHOME
++ '[' -z '' ']'
++ _OLD_VIRTUAL_PS1=
++ PS1='(ESP_venv) '
++ export PS1
++ alias pydoc
++ true
++ hash -r
+ pip_install pip
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.0)
+ pip_install f90nml
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade f90nml
Collecting f90nml
  Using cached f90nml-1.4.4-py2.py3-none-any.whl.metadata (6.0 kB)
Using cached f90nml-1.4.4-py2.py3-none-any.whl (32 kB)
Installing collected packages: f90nml
Successfully installed f90nml-1.4.4
+ pip_install numpy
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
  Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (19.3 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.0
+ pip_install openmdao
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
  Using cached openmdao-3.33.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
  Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Collecting numpy<2 (from openmdao)
  Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Collecting packaging (from openmdao)
  Using cached packaging-24.1-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
  Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
  Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
  Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
  Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
  Using cached urllib3-2.2.2-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
  Using cached certifi-2024.6.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Using cached packaging-24.1-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB)
Using cached certifi-2024.6.2-py3-none-any.whl (164 kB)
Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (140 kB)
Using cached idna-3.7-py3-none-any.whl (66 kB)
Using cached urllib3-2.2.2-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, packaging, numpy, networkx, idna, charset-normalizer, certifi, scipy, requests, openmdao
  Attempting uninstall: numpy
    Found existing installation: numpy 2.0.0
    Uninstalling numpy-2.0.0:
      Successfully uninstalled numpy-2.0.0
Successfully installed certifi-2024.6.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 numpy-1.26.4 openmdao-3.33.0 packaging-24.1 requests-2.32.3 scipy-1.13.1 urllib3-2.2.2
+ [[ reynolds == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade cvxopt
Collecting cvxopt
  Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (1.3 kB)
Using cached cvxopt-1.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (13.6 MB)
Installing collected packages: cvxopt
Successfully installed cvxopt-1.3.2
+ pip_install dill
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade dill
Collecting dill
  Using cached dill-0.3.8-py3-none-any.whl.metadata (10 kB)
Using cached dill-0.3.8-py3-none-any.whl (116 kB)
Installing collected packages: dill
Successfully installed dill-0.3.8
+ pip_install packaging
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade packaging
Requirement already satisfied: packaging in ./ESP_venv/lib/python3.11/site-packages (24.1)
+ pip_install matplotlib
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
  Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
  Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
  Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
  Using cached fonttools-4.53.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (162 kB)
Collecting kiwisolver>=1.3.1 (from matplotlib)
  Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (6.4 kB)
Requirement already satisfied: numpy>=1.23 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (1.26.4)
Requirement already satisfied: packaging>=20.0 in ./ESP_venv/lib/python3.11/site-packages (from matplotlib) (24.1)
Collecting pillow>=8 (from matplotlib)
  Using cached pillow-10.3.0-cp311-cp311-manylinux_2_28_x86_64.whl.metadata (9.2 kB)
Collecting pyparsing>=2.3.1 (from matplotlib)
  Using cached pyparsing-3.1.2-py3-none-any.whl.metadata (5.1 kB)
Collecting python-dateutil>=2.7 (from matplotlib)
  Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl.metadata (8.4 kB)
Collecting six>=1.5 (from python-dateutil>=2.7->matplotlib)
  Using cached six-1.16.0-py2.py3-none-any.whl.metadata (1.8 kB)
Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (8.3 MB)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (306 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.53.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.9 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (1.4 MB)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_28_x86_64.whl (4.5 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.53.0 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.13.1)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-06-18 21:16:51--  https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
Resolving acdl.mit.edu (acdl.mit.edu)... 18.18.33.14
Connecting to acdl.mit.edu (acdl.mit.edu)|18.18.33.14|:443... connected.
HTTP request sent, awaiting response... 200 OK
Length: 272159479 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’

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 30750K .......... .......... .......... .......... .......... 11% 59.1M 20s
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 33650K .......... .......... .......... .......... .......... 12% 12.1M 20s
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 33750K .......... .......... .......... .......... .......... 12% 11.3M 20s
 33800K .......... .......... .......... .......... .......... 12% 11.2M 20s
 33850K .......... .......... .......... .......... .......... 12% 11.9M 20s
 33900K .......... .......... .......... .......... .......... 12% 13.5M 20s
 33950K .......... .......... .......... .......... .......... 12% 12.3M 20s
 34000K .......... .......... .......... .......... .......... 12% 14.4M 20s
 34050K .......... .......... .......... .......... .......... 12% 13.5M 20s
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 34150K .......... .......... .......... .......... .......... 12% 11.8M 20s
 34200K .......... .......... .......... .......... .......... 12% 9.97M 20s
 34250K .......... .......... .......... .......... .......... 12% 11.0M 20s
 34300K .......... .......... .......... .......... .......... 12% 11.6M 20s
 34350K .......... .......... .......... .......... .......... 12% 10.2M 20s
 34400K .......... .......... .......... .......... .......... 12% 11.4M 20s
 34450K .......... .......... .......... .......... .......... 12% 11.9M 20s
 34500K .......... .......... .......... .......... .......... 12% 12.6M 20s
 34550K .......... .......... .......... .......... .......... 13% 14.8M 20s
 34600K .......... .......... .......... .......... .......... 13% 10.5M 20s
 34650K .......... .......... .......... .......... .......... 13% 12.1M 20s
 34700K .......... .......... .......... .......... .......... 13% 12.0M 20s
 34750K .......... .......... .......... .......... .......... 13% 11.8M 20s
 34800K .......... .......... .......... .......... .......... 13% 13.1M 20s
 34850K .......... .......... .......... .......... .......... 13% 11.3M 20s
 34900K .......... .......... .......... .......... .......... 13% 20.6M 19s
 34950K .......... .......... .......... .......... .......... 13% 10.7M 19s
 35000K .......... .......... .......... .......... .......... 13% 12.6M 19s
 35050K .......... .......... .......... .......... .......... 13% 8.66M 19s
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 35200K .......... .......... .......... .......... .......... 13% 8.93M 19s
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 35350K .......... .......... .......... .......... .......... 13% 9.34M 19s
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 35500K .......... .......... .......... .......... .......... 13% 12.8M 19s
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 35600K .......... .......... .......... .......... .......... 13% 8.25M 19s
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 35700K .......... .......... .......... .......... .......... 13% 10.6M 19s
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 35800K .......... .......... .......... .......... .......... 13% 7.61M 20s
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 35900K .......... .......... .......... .......... .......... 13% 16.7M 19s
 35950K .......... .......... .......... .......... .......... 13% 9.94M 19s
 36000K .......... .......... .......... .......... .......... 13% 8.78M 20s
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 36100K .......... .......... .......... .......... .......... 13% 13.8M 19s
 36150K .......... .......... .......... .......... .......... 13% 10.0M 19s
 36200K .......... .......... .......... .......... .......... 13% 9.32M 20s
 36250K .......... .......... .......... .......... .......... 13% 7.84M 20s
 36300K .......... .......... .......... .......... .......... 13% 19.0M 19s
 36350K .......... .......... .......... .......... .......... 13% 8.59M 19s
 36400K .......... .......... .......... .......... .......... 13% 8.07M 20s
 36450K .......... .......... .......... .......... .......... 13% 11.1M 20s
 36500K .......... .......... .......... .......... .......... 13% 12.8M 19s
 36550K .......... .......... .......... .......... .......... 13% 7.42M 20s
 36600K .......... .......... .......... .......... .......... 13% 11.3M 20s
 36650K .......... .......... .......... .......... .......... 13% 11.8M 19s
 36700K .......... .......... .......... .......... .......... 13% 7.81M 20s
 36750K .......... .......... .......... .......... .......... 13% 9.30M 20s
 36800K .......... .......... .......... .......... .......... 13% 13.8M 19s
 36850K .......... .......... .......... .......... .......... 13% 7.11M 20s
 36900K .......... .......... .......... .......... .......... 13% 9.51M 20s
 36950K .......... .......... .......... .......... .......... 13% 12.8M 20s
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 37100K .......... .......... .......... .......... .......... 13% 12.9M 20s
 37150K .......... .......... .......... .......... .......... 13% 12.5M 20s
 37200K .......... .......... .......... .......... .......... 14% 20.1M 19s
 37250K .......... .......... .......... .......... .......... 14% 32.2M 19s
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 37700K .......... .......... .......... .......... .......... 14% 10.4M 19s
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 37900K .......... .......... .......... .......... .......... 14% 57.4M 19s
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 38100K .......... .......... .......... .......... .......... 14% 11.4M 19s
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 38200K .......... .......... .......... .......... .......... 14% 20.6M 19s
 38250K .......... .......... .......... .......... .......... 14% 78.5M 19s
 38300K .......... .......... .......... .......... .......... 14% 12.6M 19s
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 38400K .......... .......... .......... .......... .......... 14% 29.3M 19s
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 38500K .......... .......... .......... .......... .......... 14% 9.50M 19s
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 38600K .......... .......... .......... .......... .......... 14% 8.78M 19s
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 38700K .......... .......... .......... .......... .......... 14% 8.95M 19s
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 38800K .......... .......... .......... .......... .......... 14% 11.8M 19s
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 38900K .......... .......... .......... .......... .......... 14% 19.3M 19s
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 39200K .......... .......... .......... .......... .......... 14% 9.04M 19s
 39250K .......... .......... .......... .......... .......... 14% 19.5M 19s
 39300K .......... .......... .......... .......... .......... 14% 11.5M 19s
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 39850K .......... .......... .......... .......... .......... 15% 8.85M 19s
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 40200K .......... .......... .......... .......... .......... 15% 9.87M 19s
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 40500K .......... .......... .......... .......... .......... 15% 25.0M 19s
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 40700K .......... .......... .......... .......... .......... 15% 11.7M 19s
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 40800K .......... .......... .......... .......... .......... 15% 12.8M 19s
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 41000K .......... .......... .......... .......... .......... 15% 24.4M 19s
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 41150K .......... .......... .......... .......... .......... 15% 11.3M 19s
 41200K .......... .......... .......... .......... .......... 15% 20.6M 19s
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 41400K .......... .......... .......... .......... .......... 15% 21.2M 19s
 41450K .......... .......... .......... .......... .......... 15% 11.5M 19s
 41500K .......... .......... .......... .......... .......... 15% 4.94M 19s
 41550K .......... .......... .......... .......... .......... 15%  141M 19s
 41600K .......... .......... .......... .......... .......... 15% 52.5M 19s
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 41850K .......... .......... .......... .......... .......... 15% 11.6M 19s
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 42150K .......... .......... .......... .......... .......... 15% 9.16M 19s
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 42250K .......... .......... .......... .......... .......... 15% 11.2M 19s
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 43150K .......... .......... .......... .......... .......... 16% 10.8M 19s
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 43250K .......... .......... .......... .......... .......... 16% 8.69M 19s
 43300K .......... .......... .......... .......... .......... 16% 29.9M 19s
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 44150K .......... .......... .......... .......... .......... 16% 25.2M 19s
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 44250K .......... .......... .......... .......... .......... 16% 49.5M 18s
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 44900K .......... .......... .......... .......... .......... 16% 71.7M 18s
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 45100K .......... .......... .......... .......... .......... 16% 56.4M 18s
 45150K .......... .......... .......... .......... .......... 17% 16.0M 18s
 45200K .......... .......... .......... .......... .......... 17% 25.6M 18s
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 45300K .......... .......... .......... .......... .......... 17% 29.0M 18s
 45350K .......... .......... .......... .......... .......... 17% 32.8M 18s
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 45500K .......... .......... .......... .......... .......... 17% 30.8M 18s
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 45800K .......... .......... .......... .......... .......... 17% 33.8M 18s
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 46000K .......... .......... .......... .......... .......... 17% 33.2M 18s
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 46100K .......... .......... .......... .......... .......... 17% 28.9M 18s
 46150K .......... .......... .......... .......... .......... 17% 88.0M 18s
 46200K .......... .......... .......... .......... .......... 17% 15.0M 18s
 46250K .......... .......... .......... .......... .......... 17% 13.5M 18s
 46300K .......... .......... .......... .......... .......... 17% 22.8M 18s
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 46700K .......... .......... .......... .......... .......... 17% 21.6M 18s
 46750K .......... .......... .......... .......... .......... 17% 34.5M 18s
 46800K .......... .......... .......... .......... .......... 17% 20.0M 18s
 46850K .......... .......... .......... .......... .......... 17% 28.7M 18s
 46900K .......... .......... .......... .......... .......... 17% 20.5M 18s
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 47000K .......... .......... .......... .......... .......... 17% 16.7M 18s
 47050K .......... .......... .......... .......... .......... 17% 28.9M 18s
 47100K .......... .......... .......... .......... .......... 17% 17.6M 18s
 47150K .......... .......... .......... .......... .......... 17% 33.3M 18s
 47200K .......... .......... .......... .......... .......... 17% 17.9M 18s
 47250K .......... .......... .......... .......... .......... 17% 48.7M 18s
 47300K .......... .......... .......... .......... .......... 17% 14.2M 18s
 47350K .......... .......... .......... .......... .......... 17% 31.4M 18s
 47400K .......... .......... .......... .......... .......... 17% 11.0M 18s
 47450K .......... .......... .......... .......... .......... 17% 13.1M 18s
 47500K .......... .......... .......... .......... .......... 17% 48.2M 18s
 47550K .......... .......... .......... .......... .......... 17% 13.3M 18s
 47600K .......... .......... .......... .......... .......... 17% 9.66M 18s
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 47700K .......... .......... .......... .......... .......... 17% 13.2M 18s
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 47800K .......... .......... .......... .......... .......... 18% 20.1M 18s
 47850K .......... .......... .......... .......... .......... 18% 11.3M 18s
 47900K .......... .......... .......... .......... .......... 18% 14.0M 18s
 47950K .......... .......... .......... .......... .......... 18% 11.4M 18s
 48000K .......... .......... .......... .......... .......... 18% 12.9M 18s
 48050K .......... .......... .......... .......... .......... 18% 17.3M 18s
 48100K .......... .......... .......... .......... .......... 18% 11.0M 18s
 48150K .......... .......... .......... .......... .......... 18% 16.8M 18s
 48200K .......... .......... .......... .......... .......... 18% 12.0M 18s
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 76950K .......... .......... .......... .......... .......... 28% 6.96M 15s
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 77050K .......... .......... .......... .......... .......... 29% 11.1M 15s
 77100K .......... .......... .......... .......... .......... 29% 3.69M 15s
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 82150K .......... .......... .......... .......... .......... 30% 5.72M 16s
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 91000K .......... .......... .......... .......... .......... 34% 3.41M 17s
 91050K .......... .......... .......... .......... .......... 34% 6.20M 17s
 91100K .......... .......... .......... .......... .......... 34% 5.43M 17s
 91150K .......... .......... .......... .......... .......... 34% 5.98M 17s
 91200K .......... .......... .......... .......... .......... 34% 5.52M 17s
 91250K .......... .......... .......... .......... .......... 34% 5.62M 17s
 91300K .......... .......... .......... .......... .......... 34% 5.55M 17s
 91350K .......... .......... .......... .......... .......... 34% 4.92M 17s
 91400K .......... .......... .......... .......... .......... 34% 5.67M 17s
 91450K .......... .......... .......... .......... .......... 34% 3.02M 17s
 91500K .......... .......... .......... .......... .......... 34% 5.92M 17s
 91550K .......... .......... .......... .......... .......... 34% 2.84M 17s
 91600K .......... .......... .......... .......... .......... 34% 6.45M 17s
 91650K .......... .......... .......... .......... .......... 34% 5.62M 17s
 91700K .......... .......... .......... .......... .......... 34% 5.43M 17s
 91750K .......... .......... .......... .......... .......... 34% 3.24M 17s
 91800K .......... .......... .......... .......... .......... 34% 4.93M 17s
 91850K .......... .......... .......... .......... .......... 34% 3.23M 18s
 91900K .......... .......... .......... .......... .......... 34% 5.73M 18s
 91950K .......... .......... .......... .......... .......... 34% 5.24M 18s
 92000K .......... .......... .......... .......... .......... 34% 5.15M 18s
 92050K .......... .......... .......... .......... .......... 34% 3.41M 18s
 92100K .......... .......... .......... .......... .......... 34% 5.01M 18s
 92150K .......... .......... .......... .......... .......... 34% 5.34M 18s
 92200K .......... .......... .......... .......... .......... 34% 3.27M 18s
 92250K .......... .......... .......... .......... .......... 34% 5.87M 18s
 92300K .......... .......... .......... .......... .......... 34% 5.46M 18s
 92350K .......... .......... .......... .......... .......... 34% 5.89M 18s
 92400K .......... .......... .......... .......... .......... 34% 6.18M 18s
 92450K .......... .......... .......... .......... .......... 34% 3.40M 18s
 92500K .......... .......... .......... .......... .......... 34% 5.91M 18s
 92550K .......... .......... .......... .......... .......... 34% 6.01M 18s
 92600K .......... .......... .......... .......... .......... 34% 5.78M 18s
 92650K .......... .......... .......... .......... .......... 34% 6.16M 18s
 92700K .......... .......... .......... .......... .......... 34% 3.14M 18s
 92750K .......... .......... .......... .......... .......... 34% 6.25M 18s
 92800K .......... .......... .......... .......... .......... 34% 39.2M 18s
 92850K .......... .......... .......... .......... .......... 34% 6.35M 18s
 92900K .......... .......... .......... .......... .......... 34% 5.92M 18s
 92950K .......... .......... .......... .......... .......... 34% 5.56M 18s
 93000K .......... .......... .......... .......... .......... 35% 5.69M 18s
 93050K .......... .......... .......... .......... .......... 35% 6.29M 18s
 93100K .......... .......... .......... .......... .......... 35% 5.68M 18s
 93150K .......... .......... .......... .......... .......... 35% 5.67M 18s
 93200K .......... .......... .......... .......... .......... 35% 2.95M 18s
 93250K .......... .......... .......... .......... .......... 35%  141M 18s
 93300K .......... .......... .......... .......... .......... 35% 6.82M 18s
 93350K .......... .......... .......... .......... .......... 35% 4.02M 18s
 93400K .......... .......... .......... .......... .......... 35% 6.41M 18s
 93450K .......... .......... .......... .......... .......... 35% 5.19M 18s
 93500K .......... .......... .......... .......... .......... 35% 5.98M 18s
 93550K .......... .......... .......... .......... .......... 35% 6.12M 18s
 93600K .......... .......... .......... .......... .......... 35% 3.77M 18s
 93650K .......... .......... .......... .......... .......... 35% 5.30M 18s
 93700K .......... .......... .......... .......... .......... 35% 4.89M 18s
 93750K .......... .......... .......... .......... .......... 35% 5.41M 18s
 93800K .......... .......... .......... .......... .......... 35% 5.40M 18s
 93850K .......... .......... .......... .......... .......... 35% 4.88M 18s
 93900K .......... .......... .......... .......... .......... 35% 5.05M 18s
 93950K .......... .......... .......... .......... .......... 35% 1.03M 18s
 94000K .......... .......... .......... .......... .......... 35% 20.4M 18s
 94050K .......... .......... .......... .......... .......... 35% 5.89M 18s
 94100K .......... .......... .......... .......... .......... 35% 5.54M 18s
 94150K .......... .......... .......... .......... .......... 35% 5.75M 18s
 94200K .......... .......... .......... .......... .......... 35% 5.56M 18s
 94250K .......... .......... .......... .......... .......... 35% 5.78M 18s
 94300K .......... .......... .......... .......... .......... 35% 5.49M 18s
 94350K .......... .......... .......... .......... .......... 35% 5.33M 18s
 94400K .......... .......... .......... .......... .......... 35% 5.11M 18s
 94450K .......... .......... .......... .......... .......... 35% 4.72M 18s
 94500K .......... .......... .......... .......... .......... 35% 3.20M 18s
 94550K .......... .......... .......... .......... .......... 35% 20.8M 18s
 94600K .......... .......... .......... .......... .......... 35% 2.92M 18s
 94650K .......... .......... .......... .......... .......... 35% 5.25M 18s
 94700K .......... .......... .......... .......... .......... 35% 3.05M 18s
 94750K .......... .......... .......... .......... .......... 35% 2.98M 18s
 94800K .......... .......... .......... .......... .......... 35% 3.53M 18s
 94850K .......... .......... .......... .......... .......... 35% 2.95M 18s
 94900K .......... .......... .......... .......... .......... 35% 3.24M 18s
 94950K .......... .......... .......... .......... .......... 35% 5.36M 18s
 95000K .......... .......... .......... .......... .......... 35% 3.19M 18s
 95050K .......... .......... .......... .......... .......... 35% 6.01M 18s
 95100K .......... .......... .......... .......... .......... 35% 3.20M 18s
 95150K .......... .......... .......... .......... .......... 35% 5.36M 18s
 95200K .......... .......... .......... .......... .......... 35% 3.20M 18s
 95250K .......... .......... .......... .......... .......... 35% 5.18M 18s
 95300K .......... .......... .......... .......... .......... 35% 3.04M 18s
 95350K .......... .......... .......... .......... .......... 35% 5.63M 18s
 95400K .......... .......... .......... .......... .......... 35% 5.42M 18s
 95450K .......... .......... .......... .......... .......... 35% 3.16M 18s
 95500K .......... .......... .......... .......... .......... 35% 5.88M 18s
 95550K .......... .......... .......... .......... .......... 35% 5.60M 18s
 95600K .......... .......... .......... .......... .......... 35% 5.52M 18s
 95650K .......... .......... .......... .......... .......... 36% 3.55M 18s
 95700K .......... .......... .......... .......... .......... 36% 6.13M 18s
 95750K .......... .......... .......... .......... .......... 36% 6.14M 18s
 95800K .......... .......... .......... .......... .......... 36% 6.25M 18s
 95850K .......... .......... .......... .......... .......... 36% 6.08M 18s
 95900K .......... .......... .......... .......... .......... 36% 5.88M 18s
 95950K .......... .......... .......... .......... .......... 36% 5.33M 18s
 96000K .......... .......... .......... .......... .......... 36% 5.76M 18s
 96050K .......... .......... .......... .......... .......... 36% 5.63M 18s
 96100K .......... .......... .......... .......... .......... 36% 5.06M 18s
 96150K .......... .......... .......... .......... .......... 36% 4.96M 18s
 96200K .......... .......... .......... .......... .......... 36% 4.91M 18s
 96250K .......... .......... .......... .......... .......... 36% 5.58M 18s
 96300K .......... .......... .......... .......... .......... 36% 5.83M 18s
 96350K .......... .......... .......... .......... .......... 36% 2.44M 18s
 96400K .......... .......... .......... .......... .......... 36%  143M 18s
 96450K .......... .......... .......... .......... .......... 36% 4.62M 18s
 96500K .......... .......... .......... .......... .......... 36% 3.40M 18s
 96550K .......... .......... .......... .......... .......... 36% 6.52M 18s
 96600K .......... .......... .......... .......... .......... 36% 6.10M 18s
 96650K .......... .......... .......... .......... .......... 36% 5.08M 18s
 96700K .......... .......... .......... .......... .......... 36% 3.55M 18s
 96750K .......... .......... .......... .......... .......... 36% 5.83M 18s
 96800K .......... .......... .......... .......... .......... 36% 4.72M 18s
 96850K .......... .......... .......... .......... .......... 36% 5.67M 18s
 96900K .......... .......... .......... .......... .......... 36% 5.83M 18s
 96950K .......... .......... .......... .......... .......... 36% 3.30M 18s
 97000K .......... .......... .......... .......... .......... 36% 6.29M 18s
 97050K .......... .......... .......... .......... .......... 36% 6.23M 18s
 97100K .......... .......... .......... .......... .......... 36% 5.92M 18s
 97150K .......... .......... .......... .......... .......... 36% 5.95M 18s
 97200K .......... .......... .......... .......... .......... 36% 5.91M 18s
 97250K .......... .......... .......... .......... .......... 36% 6.46M 18s
 97300K .......... .......... .......... .......... .......... 36% 6.41M 18s
 97350K .......... .......... .......... .......... .......... 36% 6.07M 18s
 97400K .......... .......... .......... .......... .......... 36% 6.15M 18s
 97450K .......... .......... .......... .......... .......... 36% 6.10M 18s
 97500K .......... .......... .......... .......... .......... 36% 34.5M 18s
 97550K .......... .......... .......... .......... .......... 36% 5.99M 18s
 97600K .......... .......... .......... .......... .......... 36% 5.87M 18s
 97650K .......... .......... .......... .......... .......... 36% 6.41M 18s
 97700K .......... .......... .......... .......... .......... 36% 6.24M 18s
 97750K .......... .......... .......... .......... .......... 36% 3.20M 18s
 97800K .......... .......... .......... .......... .......... 36%  112M 18s
 97850K .......... .......... .......... .......... .......... 36% 5.46M 18s
 97900K .......... .......... .......... .......... .......... 36% 3.44M 18s
 97950K .......... .......... .......... .......... .......... 36% 6.35M 18s
 98000K .......... .......... .......... .......... .......... 36% 5.60M 18s
 98050K .......... .......... .......... .......... .......... 36% 6.27M 18s
 98100K .......... .......... .......... .......... .......... 36% 6.19M 18s
 98150K .......... .......... .......... .......... .......... 36% 6.23M 18s
 98200K .......... .......... .......... .......... .......... 36% 3.45M 18s
 98250K .......... .......... .......... .......... .......... 36% 5.65M 18s
 98300K .......... .......... .......... .......... .......... 37% 6.17M 18s
 98350K .......... .......... .......... .......... .......... 37% 5.42M 18s
 98400K .......... .......... .......... .......... .......... 37% 5.88M 18s
 98450K .......... .......... .......... .......... .......... 37% 6.01M 18s
 98500K .......... .......... .......... .......... .......... 37% 6.27M 18s
 98550K .......... .......... .......... .......... .......... 37% 6.44M 18s
 98600K .......... .......... .......... .......... .......... 37% 6.24M 18s
 98650K .......... .......... .......... .......... .......... 37% 6.30M 18s
 98700K .......... .......... .......... .......... .......... 37% 5.80M 18s
 98750K .......... .......... .......... .......... .......... 37% 5.84M 18s
 98800K .......... .......... .......... .......... .......... 37% 5.77M 18s
 98850K .......... .......... .......... .......... .......... 37% 5.58M 18s
 98900K .......... .......... .......... .......... .......... 37% 6.35M 18s
 98950K .......... .......... .......... .......... .......... 37% 5.75M 18s
 99000K .......... .......... .......... .......... .......... 37% 2.83M 18s
 99050K .......... .......... .......... .......... .......... 37%  141M 18s
 99100K .......... .......... .......... .......... .......... 37% 3.45M 18s
 99150K .......... .......... .......... .......... .......... 37% 5.85M 18s
 99200K .......... .......... .......... .......... .......... 37% 3.20M 18s
 99250K .......... .......... .......... .......... .......... 37% 6.21M 18s
 99300K .......... .......... .......... .......... .......... 37% 6.01M 18s
 99350K .......... .......... .......... .......... .......... 37% 5.84M 18s
 99400K .......... .......... .......... .......... .......... 37% 5.69M 18s
 99450K .......... .......... .......... .......... .......... 37% 3.09M 18s
 99500K .......... .......... .......... .......... .......... 37% 5.50M 18s
 99550K .......... .......... .......... .......... .......... 37% 4.84M 18s
 99600K .......... .......... .......... .......... .......... 37% 3.36M 18s
 99650K .......... .......... .......... .......... .......... 37% 5.72M 18s
 99700K .......... .......... .......... .......... .......... 37% 5.57M 18s
 99750K .......... .......... .......... .......... .......... 37% 5.93M 18s
 99800K .......... .......... .......... .......... .......... 37% 5.67M 18s
 99850K .......... .......... .......... .......... .......... 37% 4.98M 18s
 99900K .......... .......... .......... .......... .......... 37% 3.47M 18s
 99950K .......... .......... .......... .......... .......... 37% 5.70M 18s
100000K .......... .......... .......... .......... .......... 37% 6.02M 18s
100050K .......... .......... .......... .......... .......... 37% 6.38M 18s
100100K .......... .......... .......... .......... .......... 37% 6.20M 18s
100150K .......... .......... .......... .......... .......... 37% 6.30M 18s
100200K .......... .......... .......... .......... .......... 37% 6.17M 18s
100250K .......... .......... .......... .......... .......... 37% 5.90M 18s
100300K .......... .......... .......... .......... .......... 37% 3.05M 18s
100350K .......... .......... .......... .......... .......... 37% 47.1M 18s
100400K .......... .......... .......... .......... .......... 37% 5.69M 18s
100450K .......... .......... .......... .......... .......... 37% 3.08M 18s
100500K .......... .......... .......... .......... .......... 37% 5.95M 18s
100550K .......... .......... .......... .......... .......... 37% 5.37M 18s
100600K .......... .......... .......... .......... .......... 37% 2.89M 18s
100650K .......... .......... .......... .......... .......... 37% 6.26M 18s
100700K .......... .......... .......... .......... .......... 37% 3.20M 18s
100750K .......... .......... .......... .......... .......... 37% 3.13M 18s
100800K .......... .......... .......... .......... .......... 37% 5.55M 18s
100850K .......... .......... .......... .......... .......... 37% 2.17M 18s
100900K .......... .......... .......... .......... .......... 37% 5.65M 18s
100950K .......... .......... .......... .......... .......... 38% 3.20M 18s
101000K .......... .......... .......... .......... .......... 38% 5.38M 18s
101050K .......... .......... .......... .......... .......... 38% 5.84M 18s
101100K .......... .......... .......... .......... .......... 38% 3.52M 18s
101150K .......... .......... .......... .......... .......... 38% 5.51M 18s
101200K .......... .......... .......... .......... .......... 38% 5.22M 18s
101250K .......... .......... .......... .......... .......... 38% 6.04M 18s
101300K .......... .......... .......... .......... .......... 38% 3.43M 18s
101350K .......... .......... .......... .......... .......... 38% 3.24M 18s
101400K .......... .......... .......... .......... .......... 38% 5.36M 18s
101450K .......... .......... .......... .......... .......... 38% 2.86M 18s
101500K .......... .......... .......... .......... .......... 38% 3.31M 18s
101550K .......... .......... .......... .......... .......... 38% 5.57M 18s
101600K .......... .......... .......... .......... .......... 38% 3.13M 18s
101650K .......... .......... .......... .......... .......... 38% 5.37M 18s
101700K .......... .......... .......... .......... .......... 38% 3.15M 18s
101750K .......... .......... .......... .......... .......... 38% 5.93M 18s
101800K .......... .......... .......... .......... .......... 38% 3.37M 18s
101850K .......... .......... .......... .......... .......... 38% 5.36M 18s
101900K .......... .......... .......... .......... .......... 38% 5.58M 18s
101950K .......... .......... .......... .......... .......... 38% 3.05M 18s
102000K .......... .......... .......... .......... .......... 38% 5.78M 18s
102050K .......... .......... .......... .......... .......... 38% 6.07M 18s
102100K .......... .......... .......... .......... .......... 38% 5.35M 18s
102150K .......... .......... .......... .......... .......... 38% 5.86M 18s
102200K .......... .......... .......... .......... .......... 38% 3.20M 18s
102250K .......... .......... .......... .......... .......... 38% 6.22M 18s
102300K .......... .......... .......... .......... .......... 38% 6.31M 18s
102350K .......... .......... .......... .......... .......... 38% 5.57M 18s
102400K .......... .......... .......... .......... .......... 38% 5.89M 18s
102450K .......... .......... .......... .......... .......... 38% 5.57M 18s
102500K .......... .......... .......... .......... .......... 38% 3.61M 18s
102550K .......... .......... .......... .......... .......... 38% 5.85M 18s
102600K .......... .......... .......... .......... .......... 38% 5.93M 18s
102650K .......... .......... .......... .......... .......... 38% 3.18M 18s
102700K .......... .......... .......... .......... .......... 38% 5.36M 18s
102750K .......... .......... .......... .......... .......... 38% 3.29M 18s
102800K .......... .......... .......... .......... .......... 38% 4.79M 18s
102850K .......... .......... .......... .......... .......... 38% 3.01M 18s
102900K .......... .......... .......... .......... .......... 38% 6.02M 18s
102950K .......... .......... .......... .......... .......... 38% 4.90M 18s
103000K .......... .......... .......... .......... .......... 38% 2.10M 18s
103050K .......... .......... .......... .......... .......... 38% 48.7M 18s
103100K .......... .......... .......... .......... .......... 38% 3.04M 18s
103150K .......... .......... .......... .......... .......... 38% 4.92M 18s
103200K .......... .......... .......... .......... .......... 38% 2.13M 18s
103250K .......... .......... .......... .......... .......... 38% 2.93M 18s
103300K .......... .......... .......... .......... .......... 38% 3.13M 18s
103350K .......... .......... .......... .......... .......... 38% 3.32M 18s
103400K .......... .......... .......... .......... .......... 38% 4.30M 18s
103450K .......... .......... .......... .......... .......... 38% 4.21M 18s
103500K .......... .......... .......... .......... .......... 38% 5.66M 18s
103550K .......... .......... .......... .......... .......... 38% 6.31M 18s
103600K .......... .......... .......... .......... .......... 38% 5.90M 18s
103650K .......... .......... .......... .......... .......... 39% 6.48M 18s
103700K .......... .......... .......... .......... .......... 39% 5.29M 18s
103750K .......... .......... .......... .......... .......... 39% 8.70M 18s
103800K .......... .......... .......... .......... .......... 39% 6.65M 18s
103850K .......... .......... .......... .......... .......... 39% 8.36M 18s
103900K .......... .......... .......... .......... .......... 39% 9.27M 18s
103950K .......... .......... .......... .......... .......... 39% 7.37M 18s
104000K .......... .......... .......... .......... .......... 39% 6.51M 18s
104050K .......... .......... .......... .......... .......... 39% 16.4M 18s
104100K .......... .......... .......... .......... .......... 39% 11.0M 18s
104150K .......... .......... .......... .......... .......... 39% 5.62M 18s
104200K .......... .......... .......... .......... .......... 39% 5.24M 18s
104250K .......... .......... .......... .......... .......... 39% 5.75M 18s
104300K .......... .......... .......... .......... .......... 39% 7.57M 18s
104350K .......... .......... .......... .......... .......... 39% 4.93M 18s
104400K .......... .......... .......... .......... .......... 39% 6.84M 18s
104450K .......... .......... .......... .......... .......... 39% 7.20M 18s
104500K .......... .......... .......... .......... .......... 39% 4.90M 18s
104550K .......... .......... .......... .......... .......... 39% 6.37M 18s
104600K .......... .......... .......... .......... .......... 39% 4.33M 18s
104650K .......... .......... .......... .......... .......... 39% 6.57M 18s
104700K .......... .......... .......... .......... .......... 39% 3.38M 18s
104750K .......... .......... .......... .......... .......... 39% 11.4M 18s
104800K .......... .......... .......... .......... .......... 39% 4.01M 18s
104850K .......... .......... .......... .......... .......... 39% 3.10M 18s
104900K .......... .......... .......... .......... .......... 39% 3.23M 18s
104950K .......... .......... .......... .......... .......... 39% 2.67M 18s
105000K .......... .......... .......... .......... .......... 39% 2.71M 18s
105050K .......... .......... .......... .......... .......... 39% 3.33M 18s
105100K .......... .......... .......... .......... .......... 39% 2.98M 18s
105150K .......... .......... .......... .......... .......... 39% 3.79M 18s
105200K .......... .......... .......... .......... .......... 39% 3.81M 18s
105250K .......... .......... .......... .......... .......... 39% 4.20M 18s
105300K .......... .......... .......... .......... .......... 39% 4.85M 18s
105350K .......... .......... .......... .......... .......... 39% 3.41M 18s
105400K .......... .......... .......... .......... .......... 39% 3.24M 18s
105450K .......... .......... .......... .......... .......... 39% 3.34M 18s
105500K .......... .......... .......... .......... .......... 39% 4.07M 18s
105550K .......... .......... .......... .......... .......... 39% 5.68M 18s
105600K .......... .......... .......... .......... .......... 39% 5.46M 18s
105650K .......... .......... .......... .......... .......... 39% 5.92M 18s
105700K .......... .......... .......... .......... .......... 39% 4.67M 18s
105750K .......... .......... .......... .......... .......... 39% 4.20M 18s
105800K .......... .......... .......... .......... .......... 39% 4.59M 18s
105850K .......... .......... .......... .......... .......... 39% 3.30M 18s
105900K .......... .......... .......... .......... .......... 39% 2.94M 18s
105950K .......... .......... .......... .......... .......... 39%  430K 18s
106000K .......... .......... .......... .......... .......... 39% 2.17M 18s
106050K .......... .......... .......... .......... .......... 39% 3.64M 18s
106100K .......... .......... .......... .......... .......... 39% 2.62M 19s
106150K .......... .......... .......... .......... .......... 39% 4.29M 19s
106200K .......... .......... .......... .......... .......... 39% 3.06M 19s
106250K .......... .......... .......... .......... .......... 39% 3.34M 19s
106300K .......... .......... .......... .......... .......... 40% 3.00M 19s
106350K .......... .......... .......... .......... .......... 40% 1.26M 19s
106400K .......... .......... .......... .......... .......... 40% 2.20M 19s
106450K .......... .......... .......... .......... .......... 40% 3.60M 19s
106500K .......... .......... .......... .......... .......... 40% 7.11M 19s
106550K .......... .......... .......... .......... .......... 40% 3.51M 19s
106600K .......... .......... .......... .......... .......... 40% 3.45M 19s
106650K .......... .......... .......... .......... .......... 40% 4.00M 19s
106700K .......... .......... .......... .......... .......... 40% 3.31M 19s
106750K .......... .......... .......... .......... .......... 40% 9.89M 19s
106800K .......... .......... .......... .......... .......... 40% 6.38M 19s
106850K .......... .......... .......... .......... .......... 40% 4.35M 19s
106900K .......... .......... .......... .......... .......... 40% 4.35M 19s
106950K .......... .......... .......... .......... .......... 40% 3.38M 19s
107000K .......... .......... .......... .......... .......... 40% 2.84M 19s
107050K .......... .......... .......... .......... .......... 40% 3.77M 19s
107100K .......... .......... .......... .......... .......... 40% 4.19M 19s
107150K .......... .......... .......... .......... .......... 40% 4.24M 19s
107200K .......... .......... .......... .......... .......... 40% 4.41M 19s
107250K .......... .......... .......... .......... .......... 40% 7.23M 19s
107300K .......... .......... .......... .......... .......... 40% 14.3M 19s
107350K .......... .......... .......... .......... .......... 40% 5.24M 19s
107400K .......... .......... .......... .......... .......... 40% 12.2M 19s
107450K .......... .......... .......... .......... .......... 40% 6.33M 19s
107500K .......... .......... .......... .......... .......... 40% 8.62M 19s
107550K .......... .......... .......... .......... .......... 40% 7.37M 19s
107600K .......... .......... .......... .......... .......... 40% 5.99M 19s
107650K .......... .......... .......... .......... .......... 40% 7.49M 19s
107700K .......... .......... .......... .......... .......... 40% 15.1M 19s
107750K .......... .......... .......... .......... .......... 40% 9.40M 19s
107800K .......... .......... .......... .......... .......... 40% 17.5M 19s
107850K .......... .......... .......... .......... .......... 40% 10.3M 19s
107900K .......... .......... .......... .......... .......... 40% 9.76M 19s
107950K .......... .......... .......... .......... .......... 40% 8.88M 19s
108000K .......... .......... .......... .......... .......... 40% 12.9M 19s
108050K .......... .......... .......... .......... .......... 40% 9.49M 19s
108100K .......... .......... .......... .......... .......... 40% 12.3M 19s
108150K .......... .......... .......... .......... .......... 40% 6.55M 19s
108200K .......... .......... .......... .......... .......... 40% 7.61M 19s
108250K .......... .......... .......... .......... .......... 40% 8.74M 19s
108300K .......... .......... .......... .......... .......... 40% 5.22M 19s
108350K .......... .......... .......... .......... .......... 40% 3.84M 19s
108400K .......... .......... .......... .......... .......... 40% 5.90M 19s
108450K .......... .......... .......... .......... .......... 40% 4.42M 19s
108500K .......... .......... .......... .......... .......... 40% 8.78M 19s
108550K .......... .......... .......... .......... .......... 40% 8.83M 19s
108600K .......... .......... .......... .......... .......... 40% 5.55M 19s
108650K .......... .......... .......... .......... .......... 40% 8.76M 18s
108700K .......... .......... .......... .......... .......... 40% 8.24M 18s
108750K .......... .......... .......... .......... .......... 40% 7.97M 18s
108800K .......... .......... .......... .......... .......... 40% 6.13M 18s
108850K .......... .......... .......... .......... .......... 40% 9.40M 18s
108900K .......... .......... .......... .......... .......... 40% 8.69M 18s
108950K .......... .......... .......... .......... .......... 41% 8.20M 18s
109000K .......... .......... .......... .......... .......... 41% 10.6M 18s
109050K .......... .......... .......... .......... .......... 41% 4.83M 18s
109100K .......... .......... .......... .......... .......... 41% 8.60M 18s
109150K .......... .......... .......... .......... .......... 41% 7.34M 18s
109200K .......... .......... .......... .......... .......... 41% 5.18M 18s
109250K .......... .......... .......... .......... .......... 41% 6.27M 18s
109300K .......... .......... .......... .......... .......... 41% 5.07M 18s
109350K .......... .......... .......... .......... .......... 41% 3.23M 18s
109400K .......... .......... .......... .......... .......... 41% 4.38M 18s
109450K .......... .......... .......... .......... .......... 41% 3.53M 18s
109500K .......... .......... .......... .......... .......... 41% 2.59M 18s
109550K .......... .......... .......... .......... .......... 41% 2.09M 18s
109600K .......... .......... .......... .......... .......... 41% 1.54M 19s
109650K .......... .......... .......... .......... .......... 41% 2.65M 19s
109700K .......... .......... .......... .......... .......... 41% 5.10M 19s
109750K .......... .......... .......... .......... .......... 41% 9.56M 19s
109800K .......... .......... .......... .......... .......... 41% 8.84M 19s
109850K .......... .......... .......... .......... .......... 41% 7.21M 19s
109900K .......... .......... .......... .......... .......... 41% 7.19M 19s
109950K .......... .......... .......... .......... .......... 41% 8.09M 18s
110000K .......... .......... .......... .......... .......... 41% 10.7M 18s
110050K .......... .......... .......... .......... .......... 41% 10.8M 18s
110100K .......... .......... .......... .......... .......... 41% 7.75M 18s
110150K .......... .......... .......... .......... .......... 41% 7.79M 18s
110200K .......... .......... .......... .......... .......... 41% 3.53M 18s
110250K .......... .......... .......... .......... .......... 41% 2.18M 18s
110300K .......... .......... .......... .......... .......... 41% 2.20M 19s
110350K .......... .......... .......... .......... .......... 41% 4.80M 19s
110400K .......... .......... .......... .......... .......... 41% 6.71M 19s
110450K .......... .......... .......... .......... .......... 41% 3.65M 19s
110500K .......... .......... .......... .......... .......... 41% 3.75M 19s
110550K .......... .......... .......... .......... .......... 41% 2.91M 19s
110600K .......... .......... .......... .......... .......... 41% 5.65M 19s
110650K .......... .......... .......... .......... .......... 41% 6.86M 19s
110700K .......... .......... .......... .......... .......... 41% 5.83M 19s
110750K .......... .......... .......... .......... .......... 41% 6.98M 19s
110800K .......... .......... .......... .......... .......... 41% 7.96M 19s
110850K .......... .......... .......... .......... .......... 41% 8.13M 18s
110900K .......... .......... .......... .......... .......... 41% 9.38M 18s
110950K .......... .......... .......... .......... .......... 41% 6.05M 18s
111000K .......... .......... .......... .......... .......... 41% 7.00M 18s
111050K .......... .......... .......... .......... .......... 41% 5.92M 18s
111100K .......... .......... .......... .......... .......... 41% 3.51M 18s
111150K .......... .......... .......... .......... .......... 41% 2.38M 19s
111200K .......... .......... .......... .......... .......... 41% 2.20M 19s
111250K .......... .......... .......... .......... .......... 41% 2.50M 19s
111300K .......... .......... .......... .......... .......... 41% 1.39M 19s
111350K .......... .......... .......... .......... .......... 41% 2.69M 19s
111400K .......... .......... .......... .......... .......... 41% 12.5M 19s
111450K .......... .......... .......... .......... .......... 41% 7.02M 19s
111500K .......... .......... .......... .......... .......... 41% 5.71M 19s
111550K .......... .......... .......... .......... .......... 41% 5.78M 19s
111600K .......... .......... .......... .......... .......... 42% 4.64M 19s
111650K .......... .......... .......... .......... .......... 42% 4.33M 19s
111700K .......... .......... .......... .......... .......... 42% 4.53M 19s
111750K .......... .......... .......... .......... .......... 42% 5.22M 19s
111800K .......... .......... .......... .......... .......... 42% 6.00M 19s
111850K .......... .......... .......... .......... .......... 42% 7.24M 19s
111900K .......... .......... .......... .......... .......... 42% 6.18M 19s
111950K .......... .......... .......... .......... .......... 42% 7.56M 19s
112000K .......... .......... .......... .......... .......... 42% 5.10M 19s
112050K .......... .......... .......... .......... .......... 42% 4.91M 19s
112100K .......... .......... .......... .......... .......... 42% 4.44M 19s
112150K .......... .......... .......... .......... .......... 42% 6.88M 19s
112200K .......... .......... .......... .......... .......... 42% 8.73M 19s
112250K .......... .......... .......... .......... .......... 42% 5.51M 19s
112300K .......... .......... .......... .......... .......... 42% 7.70M 19s
112350K .......... .......... .......... .......... .......... 42% 5.27M 19s
112400K .......... .......... .......... .......... .......... 42% 5.52M 19s
112450K .......... .......... .......... .......... .......... 42% 4.36M 19s
112500K .......... .......... .......... .......... .......... 42% 3.73M 19s
112550K .......... .......... .......... .......... .......... 42% 5.25M 19s
112600K .......... .......... .......... .......... .......... 42% 3.65M 19s
112650K .......... .......... .......... .......... .......... 42% 3.44M 19s
112700K .......... .......... .......... .......... .......... 42% 2.50M 19s
112750K .......... .......... .......... .......... .......... 42% 3.03M 19s
112800K .......... .......... .......... .......... .......... 42% 2.44M 19s
112850K .......... .......... .......... .......... .......... 42% 2.70M 19s
112900K .......... .......... .......... .......... .......... 42% 3.68M 19s
112950K .......... .......... .......... .......... .......... 42% 3.07M 19s
113000K .......... .......... .......... .......... .......... 42% 5.64M 19s
113050K .......... .......... .......... .......... .......... 42% 5.51M 19s
113100K .......... .......... .......... .......... .......... 42% 8.26M 19s
113150K .......... .......... .......... .......... .......... 42% 5.65M 19s
113200K .......... .......... .......... .......... .......... 42% 5.11M 19s
113250K .......... .......... .......... .......... .......... 42% 7.01M 19s
113300K .......... .......... .......... .......... .......... 42% 7.30M 19s
113350K .......... .......... .......... .......... .......... 42% 10.9M 19s
113400K .......... .......... .......... .......... .......... 42% 18.5M 19s
113450K .......... .......... .......... .......... .......... 42% 10.7M 19s
113500K .......... .......... .......... .......... .......... 42% 12.8M 19s
113550K .......... .......... .......... .......... .......... 42% 15.5M 19s
113600K .......... .......... .......... .......... .......... 42% 12.6M 19s
113650K .......... .......... .......... .......... .......... 42% 16.3M 18s
113700K .......... .......... .......... .......... .......... 42% 12.1M 18s
113750K .......... .......... .......... .......... .......... 42% 17.2M 18s
113800K .......... .......... .......... .......... .......... 42% 17.1M 18s
113850K .......... .......... .......... .......... .......... 42% 17.2M 18s
113900K .......... .......... .......... .......... .......... 42% 21.9M 18s
113950K .......... .......... .......... .......... .......... 42% 23.5M 18s
114000K .......... .......... .......... .......... .......... 42% 17.2M 18s
114050K .......... .......... .......... .......... .......... 42% 9.54M 18s
114100K .......... .......... .......... .......... .......... 42% 23.8M 18s
114150K .......... .......... .......... .......... .......... 42% 29.8M 18s
114200K .......... .......... .......... .......... .......... 42% 14.0M 18s
114250K .......... .......... .......... .......... .......... 43% 13.6M 18s
114300K .......... .......... .......... .......... .......... 43% 19.1M 18s
114350K .......... .......... .......... .......... .......... 43% 13.1M 18s
114400K .......... .......... .......... .......... .......... 43% 14.0M 18s
114450K .......... .......... .......... .......... .......... 43% 13.2M 18s
114500K .......... .......... .......... .......... .......... 43% 9.16M 18s
114550K .......... .......... .......... .......... .......... 43% 10.3M 18s
114600K .......... .......... .......... .......... .......... 43% 10.9M 18s
114650K .......... .......... .......... .......... .......... 43% 14.0M 18s
114700K .......... .......... .......... .......... .......... 43% 8.72M 18s
114750K .......... .......... .......... .......... .......... 43% 11.4M 18s
114800K .......... .......... .......... .......... .......... 43% 8.37M 18s
114850K .......... .......... .......... .......... .......... 43% 9.28M 18s
114900K .......... .......... .......... .......... .......... 43% 10.8M 18s
114950K .......... .......... .......... .......... .......... 43% 6.45M 18s
115000K .......... .......... .......... .......... .......... 43% 9.88M 18s
115050K .......... .......... .......... .......... .......... 43% 7.99M 18s
115100K .......... .......... .......... .......... .......... 43% 6.87M 18s
115150K .......... .......... .......... .......... .......... 43% 7.76M 18s
115200K .......... .......... .......... .......... .......... 43% 7.24M 18s
115250K .......... .......... .......... .......... .......... 43% 7.61M 18s
115300K .......... .......... .......... .......... .......... 43% 6.83M 18s
115350K .......... .......... .......... .......... .......... 43% 6.93M 18s
115400K .......... .......... .......... .......... .......... 43% 9.06M 18s
115450K .......... .......... .......... .......... .......... 43% 8.71M 18s
115500K .......... .......... .......... .......... .......... 43% 5.48M 18s
115550K .......... .......... .......... .......... .......... 43% 18.6M 18s
115600K .......... .......... .......... .......... .......... 43% 6.14M 18s
115650K .......... .......... .......... .......... .......... 43% 8.26M 18s
115700K .......... .......... .......... .......... .......... 43% 7.54M 18s
115750K .......... .......... .......... .......... .......... 43% 6.52M 18s
115800K .......... .......... .......... .......... .......... 43% 9.46M 18s
115850K .......... .......... .......... .......... .......... 43% 6.76M 18s
115900K .......... .......... .......... .......... .......... 43% 5.67M 18s
115950K .......... .......... .......... .......... .......... 43% 8.54M 18s
116000K .......... .......... .......... .......... .......... 43% 8.08M 18s
116050K .......... .......... .......... .......... .......... 43% 7.69M 18s
116100K .......... .......... .......... .......... .......... 43% 6.62M 18s
116150K .......... .......... .......... .......... .......... 43% 9.15M 18s
116200K .......... .......... .......... .......... .......... 43% 8.40M 18s
116250K .......... .......... .......... .......... .......... 43% 8.53M 18s
116300K .......... .......... .......... .......... .......... 43% 10.8M 18s
116350K .......... .......... .......... .......... .......... 43% 9.05M 18s
116400K .......... .......... .......... .......... .......... 43% 13.4M 18s
116450K .......... .......... .......... .......... .......... 43% 10.8M 18s
116500K .......... .......... .......... .......... .......... 43% 12.1M 18s
116550K .......... .......... .......... .......... .......... 43% 13.5M 18s
116600K .......... .......... .......... .......... .......... 43% 12.7M 18s
116650K .......... .......... .......... .......... .......... 43% 18.5M 18s
116700K .......... .......... .......... .......... .......... 43% 9.01M 18s
116750K .......... .......... .......... .......... .......... 43% 7.77M 18s
116800K .......... .......... .......... .......... .......... 43% 7.21M 18s
116850K .......... .......... .......... .......... .......... 43% 5.67M 18s
116900K .......... .......... .......... .......... .......... 44% 5.39M 18s
116950K .......... .......... .......... .......... .......... 44% 4.75M 18s
117000K .......... .......... .......... .......... .......... 44% 3.09M 18s
117050K .......... .......... .......... .......... .......... 44% 3.80M 18s
117100K .......... .......... .......... .......... .......... 44% 4.03M 18s
117150K .......... .......... .......... .......... .......... 44% 3.97M 18s
117200K .......... .......... .......... .......... .......... 44% 3.63M 18s
117250K .......... .......... .......... .......... .......... 44% 4.20M 18s
117300K .......... .......... .......... .......... .......... 44% 6.62M 18s
117350K .......... .......... .......... .......... .......... 44% 9.83M 18s
117400K .......... .......... .......... .......... .......... 44% 7.78M 18s
117450K .......... .......... .......... .......... .......... 44% 8.64M 18s
117500K .......... .......... .......... .......... .......... 44% 9.66M 18s
117550K .......... .......... .......... .......... .......... 44% 6.86M 18s
117600K .......... .......... .......... .......... .......... 44% 4.81M 18s
117650K .......... .......... .......... .......... .......... 44% 4.71M 18s
117700K .......... .......... .......... .......... .......... 44% 5.49M 18s
117750K .......... .......... .......... .......... .......... 44% 6.30M 18s
117800K .......... .......... .......... .......... .......... 44% 8.47M 18s
117850K .......... .......... .......... .......... .......... 44% 7.07M 18s
117900K .......... .......... .......... .......... .......... 44% 20.0M 18s
117950K .......... .......... .......... .......... .......... 44% 9.66M 18s
118000K .......... .......... .......... .......... .......... 44% 14.0M 18s
118050K .......... .......... .......... .......... .......... 44% 12.0M 18s
118100K .......... .......... .......... .......... .......... 44% 12.9M 18s
118150K .......... .......... .......... .......... .......... 44% 13.6M 18s
118200K .......... .......... .......... .......... .......... 44% 10.6M 18s
118250K .......... .......... .......... .......... .......... 44% 13.5M 18s
118300K .......... .......... .......... .......... .......... 44% 8.48M 18s
118350K .......... .......... .......... .......... .......... 44% 16.4M 18s
118400K .......... .......... .......... .......... .......... 44% 10.7M 18s
118450K .......... .......... .......... .......... .......... 44% 10.6M 18s
118500K .......... .......... .......... .......... .......... 44% 8.79M 18s
118550K .......... .......... .......... .......... .......... 44% 5.26M 18s
118600K .......... .......... .......... .......... .......... 44% 4.88M 18s
118650K .......... .......... .......... .......... .......... 44% 3.75M 18s
118700K .......... .......... .......... .......... .......... 44% 3.04M 18s
118750K .......... .......... .......... .......... .......... 44% 4.20M 18s
118800K .......... .......... .......... .......... .......... 44% 8.04M 18s
118850K .......... .......... .......... .......... .......... 44% 6.61M 18s
118900K .......... .......... .......... .......... .......... 44% 7.35M 18s
118950K .......... .......... .......... .......... .......... 44% 5.60M 18s
119000K .......... .......... .......... .......... .......... 44% 4.04M 18s
119050K .......... .......... .......... .......... .......... 44% 4.67M 18s
119100K .......... .......... .......... .......... .......... 44% 3.41M 18s
119150K .......... .......... .......... .......... .......... 44% 6.44M 18s
119200K .......... .......... .......... .......... .......... 44% 4.53M 18s
119250K .......... .......... .......... .......... .......... 44% 4.96M 18s
119300K .......... .......... .......... .......... .......... 44% 7.09M 18s
119350K .......... .......... .......... .......... .......... 44% 4.27M 18s
119400K .......... .......... .......... .......... .......... 44% 11.4M 18s
119450K .......... .......... .......... .......... .......... 44% 4.50M 18s
119500K .......... .......... .......... .......... .......... 44% 5.53M 18s
119550K .......... .......... .......... .......... .......... 44% 6.32M 18s
119600K .......... .......... .......... .......... .......... 45% 4.52M 18s
119650K .......... .......... .......... .......... .......... 45% 8.64M 18s
119700K .......... .......... .......... .......... .......... 45% 8.84M 18s
119750K .......... .......... .......... .......... .......... 45% 8.16M 18s
119800K .......... .......... .......... .......... .......... 45% 13.0M 18s
119850K .......... .......... .......... .......... .......... 45% 6.00M 18s
119900K .......... .......... .......... .......... .......... 45% 6.30M 18s
119950K .......... .......... .......... .......... .......... 45% 5.43M 18s
120000K .......... .......... .......... .......... .......... 45% 5.57M 18s
120050K .......... .......... .......... .......... .......... 45% 14.2M 18s
120100K .......... .......... .......... .......... .......... 45% 5.75M 18s
120150K .......... .......... .......... .......... .......... 45% 17.7M 18s
120200K .......... .......... .......... .......... .......... 45% 6.37M 18s
120250K .......... .......... .......... .......... .......... 45% 9.46M 18s
120300K .......... .......... .......... .......... .......... 45% 6.63M 18s
120350K .......... .......... .......... .......... .......... 45% 6.70M 18s
120400K .......... .......... .......... .......... .......... 45% 4.13M 18s
120450K .......... .......... .......... .......... .......... 45% 5.00M 18s
120500K .......... .......... .......... .......... .......... 45% 4.20M 18s
120550K .......... .......... .......... .......... .......... 45% 4.24M 18s
120600K .......... .......... .......... .......... .......... 45% 7.66M 18s
120650K .......... .......... .......... .......... .......... 45% 8.17M 18s
120700K .......... .......... .......... .......... .......... 45% 4.94M 18s
120750K .......... .......... .......... .......... .......... 45% 8.93M 18s
120800K .......... .......... .......... .......... .......... 45% 5.96M 18s
120850K .......... .......... .......... .......... .......... 45% 6.36M 18s
120900K .......... .......... .......... .......... .......... 45% 9.26M 18s
120950K .......... .......... .......... .......... .......... 45% 13.0M 18s
121000K .......... .......... .......... .......... .......... 45% 8.40M 18s
121050K .......... .......... .......... .......... .......... 45% 11.3M 18s
121100K .......... .......... .......... .......... .......... 45% 6.85M 18s
121150K .......... .......... .......... .......... .......... 45% 10.4M 18s
121200K .......... .......... .......... .......... .......... 45% 6.15M 18s
121250K .......... .......... .......... .......... .......... 45% 9.23M 18s
121300K .......... .......... .......... .......... .......... 45% 6.06M 18s
121350K .......... .......... .......... .......... .......... 45% 8.18M 18s
121400K .......... .......... .......... .......... .......... 45% 5.30M 18s
121450K .......... .......... .......... .......... .......... 45% 6.55M 18s
121500K .......... .......... .......... .......... .......... 45% 5.18M 18s
121550K .......... .......... .......... .......... .......... 45% 6.31M 18s
121600K .......... .......... .......... .......... .......... 45% 4.68M 18s
121650K .......... .......... .......... .......... .......... 45% 6.04M 18s
121700K .......... .......... .......... .......... .......... 45% 6.98M 18s
121750K .......... .......... .......... .......... .......... 45% 7.56M 18s
121800K .......... .......... .......... .......... .......... 45% 8.20M 18s
121850K .......... .......... .......... .......... .......... 45% 3.70M 18s
121900K .......... .......... .......... .......... .......... 45% 33.4M 18s
121950K .......... .......... .......... .......... .......... 45% 6.08M 18s
122000K .......... .......... .......... .......... .......... 45% 4.36M 18s
122050K .......... .......... .......... .......... .......... 45% 5.94M 18s
122100K .......... .......... .......... .......... .......... 45% 4.29M 18s
122150K .......... .......... .......... .......... .......... 45% 4.81M 18s
122200K .......... .......... .......... .......... .......... 45% 5.68M 18s
122250K .......... .......... .......... .......... .......... 46% 5.97M 18s
122300K .......... .......... .......... .......... .......... 46% 3.17M 18s
122350K .......... .......... .......... .......... .......... 46% 3.03M 18s
122400K .......... .......... .......... .......... .......... 46% 4.43M 18s
122450K .......... .......... .......... .......... .......... 46% 5.36M 18s
122500K .......... .......... .......... .......... .......... 46% 8.26M 18s
122550K .......... .......... .......... .......... .......... 46% 8.07M 18s
122600K .......... .......... .......... .......... .......... 46% 5.60M 18s
122650K .......... .......... .......... .......... .......... 46% 7.73M 18s
122700K .......... .......... .......... .......... .......... 46% 7.20M 18s
122750K .......... .......... .......... .......... .......... 46% 9.56M 18s
122800K .......... .......... .......... .......... .......... 46% 10.7M 18s
122850K .......... .......... .......... .......... .......... 46% 14.8M 18s
122900K .......... .......... .......... .......... .......... 46% 18.3M 18s
122950K .......... .......... .......... .......... .......... 46% 10.4M 18s
123000K .......... .......... .......... .......... .......... 46% 10.7M 18s
123050K .......... .......... .......... .......... .......... 46% 18.1M 18s
123100K .......... .......... .......... .......... .......... 46% 10.7M 18s
123150K .......... .......... .......... .......... .......... 46% 6.94M 18s
123200K .......... .......... .......... .......... .......... 46% 8.03M 17s
123250K .......... .......... .......... .......... .......... 46% 7.73M 17s
123300K .......... .......... .......... .......... .......... 46% 6.19M 17s
123350K .......... .......... .......... .......... .......... 46% 4.67M 17s
123400K .......... .......... .......... .......... .......... 46% 3.92M 17s
123450K .......... .......... .......... .......... .......... 46% 3.20M 17s
123500K .......... .......... .......... .......... .......... 46% 5.04M 17s
123550K .......... .......... .......... .......... .......... 46% 4.47M 17s
123600K .......... .......... .......... .......... .......... 46% 5.80M 17s
123650K .......... .......... .......... .......... .......... 46% 6.57M 17s
123700K .......... .......... .......... .......... .......... 46% 3.64M 17s
123750K .......... .......... .......... .......... .......... 46% 11.7M 17s
123800K .......... .......... .......... .......... .......... 46% 11.3M 17s
123850K .......... .......... .......... .......... .......... 46% 8.81M 17s
123900K .......... .......... .......... .......... .......... 46% 5.98M 17s
123950K .......... .......... .......... .......... .......... 46% 5.19M 17s
124000K .......... .......... .......... .......... .......... 46% 5.27M 17s
124050K .......... .......... .......... .......... .......... 46% 5.59M 17s
124100K .......... .......... .......... .......... .......... 46% 6.07M 17s
124150K .......... .......... .......... .......... .......... 46% 8.95M 17s
124200K .......... .......... .......... .......... .......... 46% 9.18M 17s
124250K .......... .......... .......... .......... .......... 46% 9.79M 17s
124300K .......... .......... .......... .......... .......... 46% 12.6M 17s
124350K .......... .......... .......... .......... .......... 46% 7.40M 17s
124400K .......... .......... .......... .......... .......... 46% 8.44M 17s
124450K .......... .......... .......... .......... .......... 46% 6.45M 17s
124500K .......... .......... .......... .......... .......... 46% 6.30M 17s
124550K .......... .......... .......... .......... .......... 46% 4.37M 17s
124600K .......... .......... .......... .......... .......... 46% 3.64M 17s
124650K .......... .......... .......... .......... .......... 46% 4.65M 17s
124700K .......... .......... .......... .......... .......... 46% 7.44M 17s
124750K .......... .......... .......... .......... .......... 46% 12.2M 17s
124800K .......... .......... .......... .......... .......... 46%  130M 17s
124850K .......... .......... .......... .......... .......... 46% 15.6M 17s
124900K .......... .......... .......... .......... .......... 47% 16.4M 17s
124950K .......... .......... .......... .......... .......... 47% 15.9M 17s
125000K .......... .......... .......... .......... .......... 47% 10.3M 17s
125050K .......... .......... .......... .......... .......... 47% 13.8M 17s
125100K .......... .......... .......... .......... .......... 47% 8.30M 17s
125150K .......... .......... .......... .......... .......... 47% 7.23M 17s
125200K .......... .......... .......... .......... .......... 47% 8.65M 17s
125250K .......... .......... .......... .......... .......... 47% 9.05M 17s
125300K .......... .......... .......... .......... .......... 47% 6.56M 17s
125350K .......... .......... .......... .......... .......... 47% 6.76M 17s
125400K .......... .......... .......... .......... .......... 47% 9.24M 17s
125450K .......... .......... .......... .......... .......... 47% 5.48M 17s
125500K .......... .......... .......... .......... .......... 47% 4.30M 17s
125550K .......... .......... .......... .......... .......... 47% 3.82M 17s
125600K .......... .......... .......... .......... .......... 47% 3.30M 17s
125650K .......... .......... .......... .......... .......... 47% 2.20M 17s
125700K .......... .......... .......... .......... .......... 47% 1.84M 17s
125750K .......... .......... .......... .......... .......... 47% 3.38M 17s
125800K .......... .......... .......... .......... .......... 47% 3.40M 17s
125850K .......... .......... .......... .......... .......... 47% 2.38M 17s
125900K .......... .......... .......... .......... .......... 47% 4.99M 17s
125950K .......... .......... .......... .......... .......... 47% 4.75M 17s
126000K .......... .......... .......... .......... .......... 47% 6.25M 17s
126050K .......... .......... .......... .......... .......... 47% 4.70M 17s
126100K .......... .......... .......... .......... .......... 47% 5.75M 17s
126150K .......... .......... .......... .......... .......... 47% 4.07M 17s
126200K .......... .......... .......... .......... .......... 47% 4.72M 17s
126250K .......... .......... .......... .......... .......... 47% 3.07M 17s
126300K .......... .......... .......... .......... .......... 47% 4.45M 17s
126350K .......... .......... .......... .......... .......... 47% 3.44M 17s
126400K .......... .......... .......... .......... .......... 47% 4.83M 17s
126450K .......... .......... .......... .......... .......... 47% 6.22M 17s
126500K .......... .......... .......... .......... .......... 47% 11.8M 17s
126550K .......... .......... .......... .......... .......... 47% 10.3M 17s
126600K .......... .......... .......... .......... .......... 47% 8.84M 17s
126650K .......... .......... .......... .......... .......... 47% 5.41M 17s
126700K .......... .......... .......... .......... .......... 47% 4.48M 17s
126750K .......... .......... .......... .......... .......... 47% 4.88M 17s
126800K .......... .......... .......... .......... .......... 47% 3.49M 17s
126850K .......... .......... .......... .......... .......... 47% 7.18M 17s
126900K .......... .......... .......... .......... .......... 47% 6.13M 17s
126950K .......... .......... .......... .......... .......... 47% 8.63M 17s
127000K .......... .......... .......... .......... .......... 47% 10.5M 17s
127050K .......... .......... .......... .......... .......... 47% 7.40M 17s
127100K .......... .......... .......... .......... .......... 47% 6.58M 17s
127150K .......... .......... .......... .......... .......... 47% 8.71M 17s
127200K .......... .......... .......... .......... .......... 47% 6.66M 17s
127250K .......... .......... .......... .......... .......... 47% 5.81M 17s
127300K .......... .......... .......... .......... .......... 47% 5.17M 17s
127350K .......... .......... .......... .......... .......... 47% 3.90M 17s
127400K .......... .......... .......... .......... .......... 47% 3.14M 17s
127450K .......... .......... .......... .......... .......... 47% 3.16M 17s
127500K .......... .......... .......... .......... .......... 47% 2.86M 17s
127550K .......... .......... .......... .......... .......... 48% 5.73M 17s
127600K .......... .......... .......... .......... .......... 48% 9.99M 17s
127650K .......... .......... .......... .......... .......... 48% 11.1M 17s
127700K .......... .......... .......... .......... .......... 48% 7.39M 17s
127750K .......... .......... .......... .......... .......... 48% 7.12M 17s
127800K .......... .......... .......... .......... .......... 48% 6.72M 17s
127850K .......... .......... .......... .......... .......... 48% 5.27M 17s
127900K .......... .......... .......... .......... .......... 48% 5.84M 17s
127950K .......... .......... .......... .......... .......... 48% 6.42M 17s
128000K .......... .......... .......... .......... .......... 48% 4.93M 17s
128050K .......... .......... .......... .......... .......... 48% 5.87M 17s
128100K .......... .......... .......... .......... .......... 48% 4.55M 17s
128150K .......... .......... .......... .......... .......... 48% 6.52M 17s
128200K .......... .......... .......... .......... .......... 48% 6.05M 17s
128250K .......... .......... .......... .......... .......... 48% 6.94M 17s
128300K .......... .......... .......... .......... .......... 48% 84.0M 17s
128350K .......... .......... .......... .......... .......... 48% 7.28M 17s
128400K .......... .......... .......... .......... .......... 48% 9.94M 17s
128450K .......... .......... .......... .......... .......... 48% 7.27M 17s
128500K .......... .......... .......... .......... .......... 48% 7.03M 17s
128550K .......... .......... .......... .......... .......... 48% 5.66M 17s
128600K .......... .......... .......... .......... .......... 48% 4.62M 17s
128650K .......... .......... .......... .......... .......... 48% 4.96M 17s
128700K .......... .......... .......... .......... .......... 48% 3.59M 17s
128750K .......... .......... .......... .......... .......... 48% 7.46M 17s
128800K .......... .......... .......... .......... .......... 48% 10.5M 17s
128850K .......... .......... .......... .......... .......... 48% 10.9M 17s
128900K .......... .......... .......... .......... .......... 48% 7.54M 17s
128950K .......... .......... .......... .......... .......... 48% 6.19M 17s
129000K .......... .......... .......... .......... .......... 48% 5.94M 17s
129050K .......... .......... .......... .......... .......... 48% 5.82M 17s
129100K .......... .......... .......... .......... .......... 48% 4.68M 17s
129150K .......... .......... .......... .......... .......... 48% 3.39M 17s
129200K .......... .......... .......... .......... .......... 48% 3.83M 17s
129250K .......... .......... .......... .......... .......... 48% 3.72M 17s
129300K .......... .......... .......... .......... .......... 48% 6.99M 17s
129350K .......... .......... .......... .......... .......... 48% 9.90M 17s
129400K .......... .......... .......... .......... .......... 48% 11.1M 17s
129450K .......... .......... .......... .......... .......... 48% 8.71M 17s
129500K .......... .......... .......... .......... .......... 48% 12.0M 17s
129550K .......... .......... .......... .......... .......... 48% 7.68M 17s
129600K .......... .......... .......... .......... .......... 48% 6.22M 17s
129650K .......... .......... .......... .......... .......... 48% 6.95M 17s
129700K .......... .......... .......... .......... .......... 48% 5.31M 17s
129750K .......... .......... .......... .......... .......... 48% 5.36M 17s
129800K .......... .......... .......... .......... .......... 48% 5.60M 17s
129850K .......... .......... .......... .......... .......... 48% 7.54M 17s
129900K .......... .......... .......... .......... .......... 48% 10.8M 17s
129950K .......... .......... .......... .......... .......... 48% 8.15M 17s
130000K .......... .......... .......... .......... .......... 48% 9.27M 17s
130050K .......... .......... .......... .......... .......... 48% 7.15M 17s
130100K .......... .......... .......... .......... .......... 48% 5.80M 17s
130150K .......... .......... .......... .......... .......... 48% 6.44M 17s
130200K .......... .......... .......... .......... .......... 49% 5.82M 17s
130250K .......... .......... .......... .......... .......... 49% 5.10M 17s
130300K .......... .......... .......... .......... .......... 49% 4.38M 17s
130350K .......... .......... .......... .......... .......... 49% 2.88M 17s
130400K .......... .......... .......... .......... .......... 49% 2.45M 17s
130450K .......... .......... .......... .......... .......... 49% 1.36M 17s
130500K .......... .......... .......... .......... .......... 49% 5.09M 17s
130550K .......... .......... .......... .......... .......... 49% 10.1M 17s
130600K .......... .......... .......... .......... .......... 49% 7.58M 17s
130650K .......... .......... .......... .......... .......... 49% 8.28M 17s
130700K .......... .......... .......... .......... .......... 49% 6.09M 17s
130750K .......... .......... .......... .......... .......... 49% 8.00M 17s
130800K .......... .......... .......... .......... .......... 49% 5.91M 17s
130850K .......... .......... .......... .......... .......... 49% 6.27M 17s
130900K .......... .......... .......... .......... .......... 49% 5.72M 17s
130950K .......... .......... .......... .......... .......... 49% 7.84M 17s
131000K .......... .......... .......... .......... .......... 49% 8.90M 17s
131050K .......... .......... .......... .......... .......... 49% 18.8M 17s
131100K .......... .......... .......... .......... .......... 49% 9.54M 17s
131150K .......... .......... .......... .......... .......... 49% 13.5M 17s
131200K .......... .......... .......... .......... .......... 49% 8.23M 17s
131250K .......... .......... .......... .......... .......... 49% 11.2M 17s
131300K .......... .......... .......... .......... .......... 49% 6.22M 17s
131350K .......... .......... .......... .......... .......... 49% 5.74M 17s
131400K .......... .......... .......... .......... .......... 49% 4.85M 17s
131450K .......... .......... .......... .......... .......... 49% 6.23M 17s
131500K .......... .......... .......... .......... .......... 49% 4.56M 17s
131550K .......... .......... .......... .......... .......... 49% 3.34M 17s
131600K .......... .......... .......... .......... .......... 49% 2.61M 17s
131650K .......... .......... .......... .......... .......... 49% 1.58M 17s
131700K .......... .......... .......... .......... .......... 49% 2.58M 17s
131750K .......... .......... .......... .......... .......... 49% 11.3M 17s
131800K .......... .......... .......... .......... .......... 49% 6.74M 17s
131850K .......... .......... .......... .......... .......... 49% 4.14M 17s
131900K .......... .......... .......... .......... .......... 49% 4.33M 17s
131950K .......... .......... .......... .......... .......... 49% 4.99M 17s
132000K .......... .......... .......... .......... .......... 49% 8.97M 17s
132050K .......... .......... .......... .......... .......... 49% 16.4M 17s
132100K .......... .......... .......... .......... .......... 49% 16.5M 17s
132150K .......... .......... .......... .......... .......... 49% 16.9M 17s
132200K .......... .......... .......... .......... .......... 49% 14.7M 17s
132250K .......... .......... .......... .......... .......... 49% 14.3M 17s
132300K .......... .......... .......... .......... .......... 49% 19.9M 17s
132350K .......... .......... .......... .......... .......... 49% 8.66M 17s
132400K .......... .......... .......... .......... .......... 49% 8.83M 17s
132450K .......... .......... .......... .......... .......... 49% 8.77M 17s
132500K .......... .......... .......... .......... .......... 49% 6.87M 17s
132550K .......... .......... .......... .......... .......... 49% 6.07M 17s
132600K .......... .......... .......... .......... .......... 49% 3.95M 17s
132650K .......... .......... .......... .......... .......... 49% 7.65M 17s
132700K .......... .......... .......... .......... .......... 49% 4.64M 17s
132750K .......... .......... .......... .......... .......... 49% 5.51M 17s
132800K .......... .......... .......... .......... .......... 49% 5.31M 17s
132850K .......... .......... .......... .......... .......... 50% 3.04M 17s
132900K .......... .......... .......... .......... .......... 50% 3.82M 17s
132950K .......... .......... .......... .......... .......... 50% 3.21M 17s
133000K .......... .......... .......... .......... .......... 50% 3.25M 17s
133050K .......... .......... .......... .......... .......... 50% 4.40M 17s
133100K .......... .......... .......... .......... .......... 50% 9.59M 17s
133150K .......... .......... .......... .......... .......... 50% 9.38M 17s
133200K .......... .......... .......... .......... .......... 50% 5.40M 17s
133250K .......... .......... .......... .......... .......... 50% 6.79M 17s
133300K .......... .......... .......... .......... .......... 50% 5.05M 17s
133350K .......... .......... .......... .......... .......... 50% 4.05M 17s
133400K .......... .......... .......... .......... .......... 50% 4.92M 17s
133450K .......... .......... .......... .......... .......... 50% 10.0M 17s
133500K .......... .......... .......... .......... .......... 50% 9.93M 17s
133550K .......... .......... .......... .......... .......... 50% 22.3M 17s
133600K .......... .......... .......... .......... .......... 50% 6.59M 17s
133650K .......... .......... .......... .......... .......... 50% 8.99M 17s
133700K .......... .......... .......... .......... .......... 50% 6.94M 17s
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133800K .......... .......... .......... .......... .......... 50% 6.72M 17s
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133900K .......... .......... .......... .......... .......... 50% 8.59M 17s
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134000K .......... .......... .......... .......... .......... 50% 4.67M 17s
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134100K .......... .......... .......... .......... .......... 50% 4.78M 17s
134150K .......... .......... .......... .......... .......... 50% 4.25M 17s
134200K .......... .......... .......... .......... .......... 50% 3.74M 17s
134250K .......... .......... .......... .......... .......... 50% 3.68M 17s
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134650K .......... .......... .......... .......... .......... 50%  129M 17s
134700K .......... .......... .......... .......... .......... 50% 15.4M 17s
134750K .......... .......... .......... .......... .......... 50% 23.9M 17s
134800K .......... .......... .......... .......... .......... 50% 11.7M 17s
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135000K .......... .......... .......... .......... .......... 50% 9.89M 17s
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135100K .......... .......... .......... .......... .......... 50% 4.67M 17s
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135200K .......... .......... .......... .......... .......... 50% 3.88M 17s
135250K .......... .......... .......... .......... .......... 50% 4.20M 17s
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136000K .......... .......... .......... .......... .......... 51% 6.83M 17s
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136100K .......... .......... .......... .......... .......... 51% 4.35M 17s
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137000K .......... .......... .......... .......... .......... 51% 15.0M 16s
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137100K .......... .......... .......... .......... .......... 51% 10.1M 16s
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137250K .......... .......... .......... .......... .......... 51% 10.3M 16s
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146250K .......... .......... .......... .......... .......... 55% 12.7M 16s
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146950K .......... .......... .......... .......... .......... 55% 7.64M 16s
147000K .......... .......... .......... .......... .......... 55% 8.11M 16s
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147150K .......... .......... .......... .......... .......... 55% 6.22M 15s
147200K .......... .......... .......... .......... .......... 55% 4.42M 15s
147250K .......... .......... .......... .......... .......... 55% 6.00M 15s
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147400K .......... .......... .......... .......... .......... 55% 14.5M 15s
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147500K .......... .......... .......... .......... .......... 55% 10.1M 15s
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147600K .......... .......... .......... .......... .......... 55% 14.5M 15s
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147700K .......... .......... .......... .......... .......... 55% 9.09M 15s
147750K .......... .......... .......... .......... .......... 55% 9.10M 15s
147800K .......... .......... .......... .......... .......... 55% 10.0M 15s
147850K .......... .......... .......... .......... .......... 55% 9.08M 15s
147900K .......... .......... .......... .......... .......... 55% 10.5M 15s
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148000K .......... .......... .......... .......... .......... 55% 10.8M 15s
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148100K .......... .......... .......... .......... .......... 55% 5.00M 15s
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148200K .......... .......... .......... .......... .......... 55% 2.34M 15s
148250K .......... .......... .......... .......... .......... 55% 3.39M 15s
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149000K .......... .......... .......... .......... .......... 56% 10.3M 15s
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149250K .......... .......... .......... .......... .......... 56% 5.07M 15s
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150000K .......... .......... .......... .......... .......... 56% 3.13M 15s
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151100K .......... .......... .......... .......... .......... 56% 11.8M 15s
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152000K .......... .......... .......... .......... .......... 57% 2.95M 15s
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152150K .......... .......... .......... .......... .......... 57% 8.24M 15s
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152250K .......... .......... .......... .......... .......... 57% 7.39M 15s
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152650K .......... .......... .......... .......... .......... 57% 14.8M 15s
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152800K .......... .......... .......... .......... .......... 57% 10.5M 15s
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153000K .......... .......... .......... .......... .......... 57% 6.21M 15s
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153100K .......... .......... .......... .......... .......... 57% 3.07M 15s
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154250K .......... .......... .......... .......... .......... 58% 3.74M 15s
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154900K .......... .......... .......... .......... .......... 58% 12.5M 15s
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155000K .......... .......... .......... .......... .......... 58% 10.7M 15s
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155250K .......... .......... .......... .......... .......... 58% 4.09M 15s
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155650K .......... .......... .......... .......... .......... 58% 12.9M 15s
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155900K .......... .......... .......... .......... .......... 58% 9.32M 15s
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158900K .......... .......... .......... .......... .......... 59% 12.9M 14s
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161850K .......... .......... .......... .......... .......... 60% 10.4M 14s
161900K .......... .......... .......... .......... .......... 60% 8.56M 14s
161950K .......... .......... .......... .......... .......... 60% 8.97M 14s
162000K .......... .......... .......... .......... .......... 60% 9.97M 14s
162050K .......... .......... .......... .......... .......... 60% 7.45M 14s
162100K .......... .......... .......... .......... .......... 61% 7.87M 14s
162150K .......... .......... .......... .......... .......... 61% 7.34M 14s
162200K .......... .......... .......... .......... .......... 61% 6.39M 14s
162250K .......... .......... .......... .......... .......... 61% 5.50M 14s
162300K .......... .......... .......... .......... .......... 61% 6.45M 14s
162350K .......... .......... .......... .......... .......... 61% 3.87M 14s
162400K .......... .......... .......... .......... .......... 61% 5.22M 14s
162450K .......... .......... .......... .......... .......... 61% 6.84M 14s
162500K .......... .......... .......... .......... .......... 61% 10.5M 14s
162550K .......... .......... .......... .......... .......... 61% 10.9M 14s
162600K .......... .......... .......... .......... .......... 61% 7.85M 14s
162650K .......... .......... .......... .......... .......... 61% 10.8M 14s
162700K .......... .......... .......... .......... .......... 61% 9.52M 14s
162750K .......... .......... .......... .......... .......... 61% 13.2M 14s
162800K .......... .......... .......... .......... .......... 61% 11.2M 14s
162850K .......... .......... .......... .......... .......... 61% 11.0M 14s
162900K .......... .......... .......... .......... .......... 61% 15.2M 14s
162950K .......... .......... .......... .......... .......... 61% 9.30M 14s
163000K .......... .......... .......... .......... .......... 61% 25.8M 14s
163050K .......... .......... .......... .......... .......... 61% 14.0M 14s
163100K .......... .......... .......... .......... .......... 61% 9.91M 14s
163150K .......... .......... .......... .......... .......... 61% 13.0M 14s
163200K .......... .......... .......... .......... .......... 61% 9.51M 14s
163250K .......... .......... .......... .......... .......... 61% 9.37M 14s
163300K .......... .......... .......... .......... .......... 61% 8.13M 14s
163350K .......... .......... .......... .......... .......... 61% 6.90M 14s
163400K .......... .......... .......... .......... .......... 61% 7.98M 14s
163450K .......... .......... .......... .......... .......... 61% 6.74M 14s
163500K .......... .......... .......... .......... .......... 61% 8.26M 14s
163550K .......... .......... .......... .......... .......... 61% 10.9M 14s
163600K .......... .......... .......... .......... .......... 61% 17.4M 14s
163650K .......... .......... .......... .......... .......... 61% 9.87M 14s
163700K .......... .......... .......... .......... .......... 61% 31.1M 14s
163750K .......... .......... .......... .......... .......... 61% 9.77M 14s
163800K .......... .......... .......... .......... .......... 61% 9.91M 14s
163850K .......... .......... .......... .......... .......... 61% 4.26M 14s
163900K .......... .......... .......... .......... .......... 61% 5.07M 14s
163950K .......... .......... .......... .......... .......... 61% 4.47M 14s
164000K .......... .......... .......... .......... .......... 61% 7.14M 14s
164050K .......... .......... .......... .......... .......... 61% 5.13M 14s
164100K .......... .......... .......... .......... .......... 61% 6.32M 14s
164150K .......... .......... .......... .......... .......... 61% 4.83M 14s
164200K .......... .......... .......... .......... .......... 61% 3.64M 14s
164250K .......... .......... .......... .......... .......... 61% 3.54M 14s
164300K .......... .......... .......... .......... .......... 61% 4.21M 14s
164350K .......... .......... .......... .......... .......... 61% 4.31M 14s
164400K .......... .......... .......... .......... .......... 61% 4.59M 14s
164450K .......... .......... .......... .......... .......... 61% 3.76M 14s
164500K .......... .......... .......... .......... .......... 61% 3.56M 14s
164550K .......... .......... .......... .......... .......... 61% 3.35M 14s
164600K .......... .......... .......... .......... .......... 61% 3.35M 14s
164650K .......... .......... .......... .......... .......... 61% 3.70M 14s
164700K .......... .......... .......... .......... .......... 61% 5.09M 14s
164750K .......... .......... .......... .......... .......... 62% 18.9M 14s
164800K .......... .......... .......... .......... .......... 62% 9.35M 14s
164850K .......... .......... .......... .......... .......... 62% 9.25M 14s
164900K .......... .......... .......... .......... .......... 62% 9.82M 14s
164950K .......... .......... .......... .......... .......... 62% 6.52M 14s
165000K .......... .......... .......... .......... .......... 62% 8.22M 14s
165050K .......... .......... .......... .......... .......... 62% 8.64M 14s
165100K .......... .......... .......... .......... .......... 62% 7.24M 14s
165150K .......... .......... .......... .......... .......... 62% 8.30M 14s
165200K .......... .......... .......... .......... .......... 62% 5.93M 14s
165250K .......... .......... .......... .......... .......... 62% 4.84M 14s
165300K .......... .......... .......... .......... .......... 62% 4.11M 14s
165350K .......... .......... .......... .......... .......... 62% 2.15M 14s
165400K .......... .......... .......... .......... .......... 62% 1.94M 14s
165450K .......... .......... .......... .......... .......... 62% 6.81M 14s
165500K .......... .......... .......... .......... .......... 62% 7.74M 14s
165550K .......... .......... .......... .......... .......... 62% 9.55M 14s
165600K .......... .......... .......... .......... .......... 62% 5.22M 14s
165650K .......... .......... .......... .......... .......... 62% 6.58M 14s
165700K .......... .......... .......... .......... .......... 62% 4.24M 14s
165750K .......... .......... .......... .......... .......... 62% 5.01M 14s
165800K .......... .......... .......... .......... .......... 62% 7.53M 13s
165850K .......... .......... .......... .......... .......... 62% 6.03M 13s
165900K .......... .......... .......... .......... .......... 62% 5.10M 13s
165950K .......... .......... .......... .......... .......... 62% 4.36M 13s
166000K .......... .......... .......... .......... .......... 62% 3.43M 13s
166050K .......... .......... .......... .......... .......... 62% 3.12M 13s
166100K .......... .......... .......... .......... .......... 62% 1.94M 13s
166150K .......... .......... .......... .......... .......... 62% 1.68M 13s
166200K .......... .......... .......... .......... .......... 62% 3.27M 13s
166250K .......... .......... .......... .......... .......... 62% 6.24M 13s
166300K .......... .......... .......... .......... .......... 62% 8.10M 13s
166350K .......... .......... .......... .......... .......... 62% 6.88M 13s
166400K .......... .......... .......... .......... .......... 62% 8.36M 13s
166450K .......... .......... .......... .......... .......... 62% 6.36M 13s
166500K .......... .......... .......... .......... .......... 62% 8.19M 13s
166550K .......... .......... .......... .......... .......... 62% 21.6M 13s
166600K .......... .......... .......... .......... .......... 62% 10.3M 13s
166650K .......... .......... .......... .......... .......... 62% 12.1M 13s
166700K .......... .......... .......... .......... .......... 62% 9.67M 13s
166750K .......... .......... .......... .......... .......... 62% 6.31M 13s
166800K .......... .......... .......... .......... .......... 62% 8.93M 13s
166850K .......... .......... .......... .......... .......... 62% 6.44M 13s
166900K .......... .......... .......... .......... .......... 62% 5.97M 13s
166950K .......... .......... .......... .......... .......... 62% 10.3M 13s
167000K .......... .......... .......... .......... .......... 62% 7.50M 13s
167050K .......... .......... .......... .......... .......... 62% 9.05M 13s
167100K .......... .......... .......... .......... .......... 62% 5.60M 13s
167150K .......... .......... .......... .......... .......... 62% 4.56M 13s
167200K .......... .......... .......... .......... .......... 62% 4.50M 13s
167250K .......... .......... .......... .......... .......... 62% 4.36M 13s
167300K .......... .......... .......... .......... .......... 62% 5.01M 13s
167350K .......... .......... .......... .......... .......... 62% 3.09M 13s
167400K .......... .......... .......... .......... .......... 63% 3.71M 13s
167450K .......... .......... .......... .......... .......... 63% 7.43M 13s
167500K .......... .......... .......... .......... .......... 63% 13.4M 13s
167550K .......... .......... .......... .......... .......... 63% 12.7M 13s
167600K .......... .......... .......... .......... .......... 63% 5.02M 13s
167650K .......... .......... .......... .......... .......... 63% 5.66M 13s
167700K .......... .......... .......... .......... .......... 63% 4.64M 13s
167750K .......... .......... .......... .......... .......... 63% 4.37M 13s
167800K .......... .......... .......... .......... .......... 63% 4.85M 13s
167850K .......... .......... .......... .......... .......... 63% 3.62M 13s
167900K .......... .......... .......... .......... .......... 63% 6.11M 13s
167950K .......... .......... .......... .......... .......... 63% 11.9M 13s
168000K .......... .......... .......... .......... .......... 63% 10.5M 13s
168050K .......... .......... .......... .......... .......... 63% 11.4M 13s
168100K .......... .......... .......... .......... .......... 63% 7.14M 13s
168150K .......... .......... .......... .......... .......... 63% 6.56M 13s
168200K .......... .......... .......... .......... .......... 63% 5.09M 13s
168250K .......... .......... .......... .......... .......... 63% 6.78M 13s
168300K .......... .......... .......... .......... .......... 63% 5.07M 13s
168350K .......... .......... .......... .......... .......... 63% 4.69M 13s
168400K .......... .......... .......... .......... .......... 63% 8.12M 13s
168450K .......... .......... .......... .......... .......... 63% 5.25M 13s
168500K .......... .......... .......... .......... .......... 63% 6.71M 13s
168550K .......... .......... .......... .......... .......... 63% 10.2M 13s
168600K .......... .......... .......... .......... .......... 63% 6.29M 13s
168650K .......... .......... .......... .......... .......... 63% 13.1M 13s
168700K .......... .......... .......... .......... .......... 63% 6.63M 13s
168750K .......... .......... .......... .......... .......... 63% 21.9M 13s
168800K .......... .......... .......... .......... .......... 63% 11.9M 13s
168850K .......... .......... .......... .......... .......... 63% 11.4M 13s
168900K .......... .......... .......... .......... .......... 63% 12.4M 13s
168950K .......... .......... .......... .......... .......... 63% 11.1M 13s
169000K .......... .......... .......... .......... .......... 63% 11.1M 13s
169050K .......... .......... .......... .......... .......... 63% 8.70M 13s
169100K .......... .......... .......... .......... .......... 63% 10.5M 13s
169150K .......... .......... .......... .......... .......... 63% 13.5M 13s
169200K .......... .......... .......... .......... .......... 63% 9.38M 13s
169250K .......... .......... .......... .......... .......... 63% 13.3M 13s
169300K .......... .......... .......... .......... .......... 63% 14.0M 13s
169350K .......... .......... .......... .......... .......... 63% 24.6M 13s
169400K .......... .......... .......... .......... .......... 63% 27.4M 13s
169450K .......... .......... .......... .......... .......... 63% 22.0M 13s
169500K .......... .......... .......... .......... .......... 63% 9.50M 13s
169550K .......... .......... .......... .......... .......... 63% 88.3M 13s
169600K .......... .......... .......... .......... .......... 63% 13.5M 13s
169650K .......... .......... .......... .......... .......... 63% 15.2M 13s
169700K .......... .......... .......... .......... .......... 63% 6.83M 13s
169750K .......... .......... .......... .......... .......... 63% 13.1M 13s
169800K .......... .......... .......... .......... .......... 63% 8.62M 13s
169850K .......... .......... .......... .......... .......... 63% 8.26M 13s
169900K .......... .......... .......... .......... .......... 63% 8.47M 13s
169950K .......... .......... .......... .......... .......... 63% 12.0M 13s
170000K .......... .......... .......... .......... .......... 63% 8.08M 13s
170050K .......... .......... .......... .......... .......... 64% 11.4M 13s
170100K .......... .......... .......... .......... .......... 64% 6.88M 13s
170150K .......... .......... .......... .......... .......... 64% 11.3M 13s
170200K .......... .......... .......... .......... .......... 64% 7.28M 13s
170250K .......... .......... .......... .......... .......... 64% 11.1M 13s
170300K .......... .......... .......... .......... .......... 64% 8.08M 13s
170350K .......... .......... .......... .......... .......... 64% 6.42M 13s
170400K .......... .......... .......... .......... .......... 64% 9.86M 13s
170450K .......... .......... .......... .......... .......... 64% 6.80M 13s
170500K .......... .......... .......... .......... .......... 64% 8.81M 13s
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170650K .......... .......... .......... .......... .......... 64% 5.98M 13s
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170750K .......... .......... .......... .......... .......... 64% 4.77M 13s
170800K .......... .......... .......... .......... .......... 64% 7.57M 13s
170850K .......... .......... .......... .......... .......... 64% 7.88M 13s
170900K .......... .......... .......... .......... .......... 64% 11.5M 13s
170950K .......... .......... .......... .......... .......... 64% 8.76M 13s
171000K .......... .......... .......... .......... .......... 64% 10.0M 13s
171050K .......... .......... .......... .......... .......... 64% 10.0M 13s
171100K .......... .......... .......... .......... .......... 64% 8.97M 13s
171150K .......... .......... .......... .......... .......... 64% 10.5M 13s
171200K .......... .......... .......... .......... .......... 64% 10.8M 13s
171250K .......... .......... .......... .......... .......... 64% 13.1M 13s
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171350K .......... .......... .......... .......... .......... 64% 29.7M 13s
171400K .......... .......... .......... .......... .......... 64% 16.7M 13s
171450K .......... .......... .......... .......... .......... 64% 13.8M 13s
171500K .......... .......... .......... .......... .......... 64% 15.3M 13s
171550K .......... .......... .......... .......... .......... 64% 15.3M 13s
171600K .......... .......... .......... .......... .......... 64% 15.0M 13s
171650K .......... .......... .......... .......... .......... 64% 17.1M 13s
171700K .......... .......... .......... .......... .......... 64% 15.4M 13s
171750K .......... .......... .......... .......... .......... 64% 19.6M 13s
171800K .......... .......... .......... .......... .......... 64% 14.2M 13s
171850K .......... .......... .......... .......... .......... 64% 12.6M 13s
171900K .......... .......... .......... .......... .......... 64% 10.6M 13s
171950K .......... .......... .......... .......... .......... 64% 9.12M 13s
172000K .......... .......... .......... .......... .......... 64% 12.2M 13s
172050K .......... .......... .......... .......... .......... 64% 10.1M 13s
172100K .......... .......... .......... .......... .......... 64% 7.71M 13s
172150K .......... .......... .......... .......... .......... 64% 7.58M 13s
172200K .......... .......... .......... .......... .......... 64% 5.02M 13s
172250K .......... .......... .......... .......... .......... 64% 6.55M 13s
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172400K .......... .......... .......... .......... .......... 64% 9.49M 13s
172450K .......... .......... .......... .......... .......... 64% 7.44M 13s
172500K .......... .......... .......... .......... .......... 64% 8.99M 13s
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172600K .......... .......... .......... .......... .......... 64% 8.09M 13s
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172700K .......... .......... .......... .......... .......... 64% 5.64M 13s
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172800K .......... .......... .......... .......... .......... 65% 4.57M 13s
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172900K .......... .......... .......... .......... .......... 65% 3.53M 13s
172950K .......... .......... .......... .......... .......... 65% 3.79M 13s
173000K .......... .......... .......... .......... .......... 65% 4.15M 13s
173050K .......... .......... .......... .......... .......... 65% 2.67M 13s
173100K .......... .......... .......... .......... .......... 65% 1.62M 13s
173150K .......... .......... .......... .......... .......... 65% 2.34M 13s
173200K .......... .......... .......... .......... .......... 65% 10.6M 13s
173250K .......... .......... .......... .......... .......... 65% 6.48M 13s
173300K .......... .......... .......... .......... .......... 65% 13.9M 13s
173350K .......... .......... .......... .......... .......... 65% 8.32M 13s
173400K .......... .......... .......... .......... .......... 65% 7.28M 13s
173450K .......... .......... .......... .......... .......... 65% 7.57M 12s
173500K .......... .......... .......... .......... .......... 65% 8.77M 12s
173550K .......... .......... .......... .......... .......... 65% 8.76M 12s
173600K .......... .......... .......... .......... .......... 65% 10.0M 12s
173650K .......... .......... .......... .......... .......... 65% 43.4M 12s
173700K .......... .......... .......... .......... .......... 65% 15.4M 12s
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173800K .......... .......... .......... .......... .......... 65% 8.79M 12s
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174000K .......... .......... .......... .......... .......... 65% 7.65M 12s
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174100K .......... .......... .......... .......... .......... 65% 4.52M 12s
174150K .......... .......... .......... .......... .......... 65% 5.38M 12s
174200K .......... .......... .......... .......... .......... 65% 3.68M 12s
174250K .......... .......... .......... .......... .......... 65% 4.78M 12s
174300K .......... .......... .......... .......... .......... 65% 5.11M 12s
174350K .......... .......... .......... .......... .......... 65% 3.67M 12s
174400K .......... .......... .......... .......... .......... 65% 4.22M 12s
174450K .......... .......... .......... .......... .......... 65% 3.09M 12s
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174550K .......... .......... .......... .......... .......... 65% 2.29M 12s
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174650K .......... .......... .......... .......... .......... 65% 3.77M 12s
174700K .......... .......... .......... .......... .......... 65% 9.74M 12s
174750K .......... .......... .......... .......... .......... 65% 11.2M 12s
174800K .......... .......... .......... .......... .......... 65% 23.5M 12s
174850K .......... .......... .......... .......... .......... 65% 12.4M 12s
174900K .......... .......... .......... .......... .......... 65% 9.74M 12s
174950K .......... .......... .......... .......... .......... 65% 6.00M 12s
175000K .......... .......... .......... .......... .......... 65% 5.64M 12s
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175100K .......... .......... .......... .......... .......... 65% 4.03M 12s
175150K .......... .......... .......... .......... .......... 65% 3.38M 12s
175200K .......... .......... .......... .......... .......... 65% 1.89M 12s
175250K .......... .......... .......... .......... .......... 65% 2.57M 12s
175300K .......... .......... .......... .......... .......... 65% 8.13M 12s
175350K .......... .......... .......... .......... .......... 65% 9.53M 12s
175400K .......... .......... .......... .......... .......... 66% 10.2M 12s
175450K .......... .......... .......... .......... .......... 66% 9.77M 12s
175500K .......... .......... .......... .......... .......... 66% 6.21M 12s
175550K .......... .......... .......... .......... .......... 66% 8.24M 12s
175600K .......... .......... .......... .......... .......... 66% 4.58M 12s
175650K .......... .......... .......... .......... .......... 66% 4.27M 12s
175700K .......... .......... .......... .......... .......... 66% 3.20M 12s
175750K .......... .......... .......... .......... .......... 66% 4.45M 12s
175800K .......... .......... .......... .......... .......... 66% 4.22M 12s
175850K .......... .......... .......... .......... .......... 66% 3.42M 12s
175900K .......... .......... .......... .......... .......... 66% 4.05M 12s
175950K .......... .......... .......... .......... .......... 66% 3.28M 12s
176000K .......... .......... .......... .......... .......... 66% 2.88M 12s
176050K .......... .......... .......... .......... .......... 66% 5.13M 12s
176100K .......... .......... .......... .......... .......... 66% 3.72M 12s
176150K .......... .......... .......... .......... .......... 66% 4.42M 12s
176200K .......... .......... .......... .......... .......... 66% 6.36M 12s
176250K .......... .......... .......... .......... .......... 66% 9.85M 12s
176300K .......... .......... .......... .......... .......... 66% 7.58M 12s
176350K .......... .......... .......... .......... .......... 66% 4.84M 12s
176400K .......... .......... .......... .......... .......... 66% 3.14M 12s
176450K .......... .......... .......... .......... .......... 66% 3.57M 12s
176500K .......... .......... .......... .......... .......... 66% 4.65M 12s
176550K .......... .......... .......... .......... .......... 66% 8.19M 12s
176600K .......... .......... .......... .......... .......... 66% 9.15M 12s
176650K .......... .......... .......... .......... .......... 66% 8.85M 12s
176700K .......... .......... .......... .......... .......... 66% 8.21M 12s
176750K .......... .......... .......... .......... .......... 66% 12.0M 12s
176800K .......... .......... .......... .......... .......... 66% 11.3M 12s
176850K .......... .......... .......... .......... .......... 66% 9.22M 12s
176900K .......... .......... .......... .......... .......... 66% 20.5M 12s
176950K .......... .......... .......... .......... .......... 66% 11.9M 12s
177000K .......... .......... .......... .......... .......... 66%  133M 12s
177050K .......... .......... .......... .......... .......... 66% 14.5M 12s
177100K .......... .......... .......... .......... .......... 66% 8.66M 12s
177150K .......... .......... .......... .......... .......... 66% 74.7M 12s
177200K .......... .......... .......... .......... .......... 66% 12.8M 12s
177250K .......... .......... .......... .......... .......... 66% 13.4M 12s
177300K .......... .......... .......... .......... .......... 66% 9.64M 12s
177350K .......... .......... .......... .......... .......... 66% 10.4M 12s
177400K .......... .......... .......... .......... .......... 66% 15.1M 12s
177450K .......... .......... .......... .......... .......... 66% 10.2M 12s
177500K .......... .......... .......... .......... .......... 66% 9.97M 12s
177550K .......... .......... .......... .......... .......... 66% 7.03M 12s
177600K .......... .......... .......... .......... .......... 66% 5.92M 12s
177650K .......... .......... .......... .......... .......... 66% 7.47M 12s
177700K .......... .......... .......... .......... .......... 66% 6.09M 12s
177750K .......... .......... .......... .......... .......... 66% 9.96M 12s
177800K .......... .......... .......... .......... .......... 66% 10.5M 12s
177850K .......... .......... .......... .......... .......... 66%  111M 12s
177900K .......... .......... .......... .......... .......... 66% 10.5M 12s
177950K .......... .......... .......... .......... .......... 66% 17.5M 12s
178000K .......... .......... .......... .......... .......... 66% 11.6M 12s
178050K .......... .......... .......... .......... .......... 67% 8.73M 12s
178100K .......... .......... .......... .......... .......... 67% 14.3M 12s
178150K .......... .......... .......... .......... .......... 67% 8.30M 12s
178200K .......... .......... .......... .......... .......... 67% 5.86M 12s
178250K .......... .......... .......... .......... .......... 67% 6.44M 12s
178300K .......... .......... .......... .......... .......... 67% 8.70M 12s
178350K .......... .......... .......... .......... .......... 67% 6.14M 12s
178400K .......... .......... .......... .......... .......... 67% 8.24M 12s
178450K .......... .......... .......... .......... .......... 67% 5.25M 12s
178500K .......... .......... .......... .......... .......... 67% 4.23M 12s
178550K .......... .......... .......... .......... .......... 67% 3.44M 12s
178600K .......... .......... .......... .......... .......... 67% 2.78M 12s
178650K .......... .......... .......... .......... .......... 67% 3.34M 12s
178700K .......... .......... .......... .......... .......... 67% 3.05M 12s
178750K .......... .......... .......... .......... .......... 67% 5.23M 12s
178800K .......... .......... .......... .......... .......... 67% 4.57M 12s
178850K .......... .......... .......... .......... .......... 67% 5.62M 12s
178900K .......... .......... .......... .......... .......... 67% 6.21M 12s
178950K .......... .......... .......... .......... .......... 67% 3.26M 12s
179000K .......... .......... .......... .......... .......... 67% 2.82M 12s
179050K .......... .......... .......... .......... .......... 67% 2.80M 12s
179100K .......... .......... .......... .......... .......... 67% 4.99M 12s
179150K .......... .......... .......... .......... .......... 67% 11.4M 12s
179200K .......... .......... .......... .......... .......... 67% 6.02M 12s
179250K .......... .......... .......... .......... .......... 67% 7.30M 12s
179300K .......... .......... .......... .......... .......... 67% 7.80M 12s
179350K .......... .......... .......... .......... .......... 67% 7.12M 12s
179400K .......... .......... .......... .......... .......... 67% 6.40M 12s
179450K .......... .......... .......... .......... .......... 67% 4.25M 12s
179500K .......... .......... .......... .......... .......... 67% 4.09M 12s
179550K .......... .......... .......... .......... .......... 67% 4.04M 12s
179600K .......... .......... .......... .......... .......... 67% 2.79M 12s
179650K .......... .......... .......... .......... .......... 67%  822K 12s
179700K .......... .......... .......... .......... .......... 67% 3.83M 12s
179750K .......... .......... .......... .......... .......... 67% 4.53M 12s
179800K .......... .......... .......... .......... .......... 67% 4.66M 12s
179850K .......... .......... .......... .......... .......... 67% 9.74M 12s
179900K .......... .......... .......... .......... .......... 67% 18.8M 12s
179950K .......... .......... .......... .......... .......... 67% 12.6M 12s
180000K .......... .......... .......... .......... .......... 67% 7.96M 12s
180050K .......... .......... .......... .......... .......... 67% 20.9M 12s
180100K .......... .......... .......... .......... .......... 67% 6.62M 12s
180150K .......... .......... .......... .......... .......... 67% 6.93M 12s
180200K .......... .......... .......... .......... .......... 67% 7.66M 12s
180250K .......... .......... .......... .......... .......... 67% 7.79M 12s
180300K .......... .......... .......... .......... .......... 67% 4.55M 12s
180350K .......... .......... .......... .......... .......... 67% 4.17M 12s
180400K .......... .......... .......... .......... .......... 67% 5.21M 12s
180450K .......... .......... .......... .......... .......... 67% 5.60M 12s
180500K .......... .......... .......... .......... .......... 67% 8.59M 12s
180550K .......... .......... .......... .......... .......... 67% 10.9M 12s
180600K .......... .......... .......... .......... .......... 67% 7.72M 12s
180650K .......... .......... .......... .......... .......... 67% 8.24M 12s
180700K .......... .......... .......... .......... .......... 68% 7.87M 12s
180750K .......... .......... .......... .......... .......... 68% 8.80M 12s
180800K .......... .......... .......... .......... .......... 68% 8.36M 12s
180850K .......... .......... .......... .......... .......... 68% 5.70M 12s
180900K .......... .......... .......... .......... .......... 68% 23.4M 12s
180950K .......... .......... .......... .......... .......... 68% 17.4M 12s
181000K .......... .......... .......... .......... .......... 68% 14.4M 12s
181050K .......... .......... .......... .......... .......... 68% 22.5M 12s
181100K .......... .......... .......... .......... .......... 68% 9.74M 12s
181150K .......... .......... .......... .......... .......... 68% 15.9M 12s
181200K .......... .......... .......... .......... .......... 68% 10.2M 12s
181250K .......... .......... .......... .......... .......... 68% 7.80M 12s
181300K .......... .......... .......... .......... .......... 68% 6.33M 12s
181350K .......... .......... .......... .......... .......... 68% 5.90M 12s
181400K .......... .......... .......... .......... .......... 68% 6.48M 12s
181450K .......... .......... .......... .......... .......... 68% 4.84M 12s
181500K .......... .......... .......... .......... .......... 68% 3.81M 12s
181550K .......... .......... .......... .......... .......... 68% 3.90M 12s
181600K .......... .......... .......... .......... .......... 68% 2.35M 12s
181650K .......... .......... .......... .......... .......... 68% 3.17M 12s
181700K .......... .......... .......... .......... .......... 68% 2.12M 12s
181750K .......... .......... .......... .......... .......... 68% 2.96M 12s
181800K .......... .......... .......... .......... .......... 68% 15.1M 12s
181850K .......... .......... .......... .......... .......... 68% 23.2M 11s
181900K .......... .......... .......... .......... .......... 68% 16.0M 11s
181950K .......... .......... .......... .......... .......... 68% 14.9M 11s
182000K .......... .......... .......... .......... .......... 68% 17.7M 11s
182050K .......... .......... .......... .......... .......... 68% 11.6M 11s
182100K .......... .......... .......... .......... .......... 68% 8.94M 11s
182150K .......... .......... .......... .......... .......... 68% 9.43M 11s
182200K .......... .......... .......... .......... .......... 68% 7.64M 11s
182250K .......... .......... .......... .......... .......... 68% 8.12M 11s
182300K .......... .......... .......... .......... .......... 68% 6.39M 11s
182350K .......... .......... .......... .......... .......... 68% 3.63M 11s
182400K .......... .......... .......... .......... .......... 68% 5.21M 11s
182450K .......... .......... .......... .......... .......... 68% 5.07M 11s
182500K .......... .......... .......... .......... .......... 68% 5.13M 11s
182550K .......... .......... .......... .......... .......... 68% 5.72M 11s
182600K .......... .......... .......... .......... .......... 68% 4.57M 11s
182650K .......... .......... .......... .......... .......... 68% 5.01M 11s
182700K .......... .......... .......... .......... .......... 68% 10.5M 11s
182750K .......... .......... .......... .......... .......... 68% 12.0M 11s
182800K .......... .......... .......... .......... .......... 68% 14.7M 11s
182850K .......... .......... .......... .......... .......... 68% 7.78M 11s
182900K .......... .......... .......... .......... .......... 68% 9.41M 11s
182950K .......... .......... .......... .......... .......... 68% 7.34M 11s
183000K .......... .......... .......... .......... .......... 68% 9.01M 11s
183050K .......... .......... .......... .......... .......... 68% 9.65M 11s
183100K .......... .......... .......... .......... .......... 68% 6.23M 11s
183150K .......... .......... .......... .......... .......... 68% 9.09M 11s
183200K .......... .......... .......... .......... .......... 68% 8.86M 11s
183250K .......... .......... .......... .......... .......... 68% 7.33M 11s
183300K .......... .......... .......... .......... .......... 68% 5.88M 11s
183350K .......... .......... .......... .......... .......... 69% 4.33M 11s
183400K .......... .......... .......... .......... .......... 69% 2.70M 11s
183450K .......... .......... .......... .......... .......... 69% 2.10M 11s
183500K .......... .......... .......... .......... .......... 69% 2.15M 11s
183550K .......... .......... .......... .......... .......... 69% 2.07M 11s
183600K .......... .......... .......... .......... .......... 69% 2.50M 11s
183650K .......... .......... .......... .......... .......... 69% 7.25M 11s
183700K .......... .......... .......... .......... .......... 69% 13.6M 11s
183750K .......... .......... .......... .......... .......... 69% 10.3M 11s
183800K .......... .......... .......... .......... .......... 69% 13.7M 11s
183850K .......... .......... .......... .......... .......... 69% 9.29M 11s
183900K .......... .......... .......... .......... .......... 69% 10.6M 11s
183950K .......... .......... .......... .......... .......... 69% 8.08M 11s
184000K .......... .......... .......... .......... .......... 69% 8.70M 11s
184050K .......... .......... .......... .......... .......... 69% 8.35M 11s
184100K .......... .......... .......... .......... .......... 69% 6.96M 11s
184150K .......... .......... .......... .......... .......... 69% 6.14M 11s
184200K .......... .......... .......... .......... .......... 69% 5.60M 11s
184250K .......... .......... .......... .......... .......... 69% 9.11M 11s
184300K .......... .......... .......... .......... .......... 69% 6.62M 11s
184350K .......... .......... .......... .......... .......... 69% 5.15M 11s
184400K .......... .......... .......... .......... .......... 69% 7.75M 11s
184450K .......... .......... .......... .......... .......... 69% 14.4M 11s
184500K .......... .......... .......... .......... .......... 69% 14.5M 11s
184550K .......... .......... .......... .......... .......... 69% 15.1M 11s
184600K .......... .......... .......... .......... .......... 69% 17.2M 11s
184650K .......... .......... .......... .......... .......... 69% 12.8M 11s
184700K .......... .......... .......... .......... .......... 69% 5.79M 11s
184750K .......... .......... .......... .......... .......... 69% 8.41M 11s
184800K .......... .......... .......... .......... .......... 69% 7.89M 11s
184850K .......... .......... .......... .......... .......... 69% 6.04M 11s
184900K .......... .......... .......... .......... .......... 69% 4.32M 11s
184950K .......... .......... .......... .......... .......... 69% 3.92M 11s
185000K .......... .......... .......... .......... .......... 69% 5.06M 11s
185050K .......... .......... .......... .......... .......... 69% 5.08M 11s
185100K .......... .......... .......... .......... .......... 69% 3.58M 11s
185150K .......... .......... .......... .......... .......... 69% 5.09M 11s
185200K .......... .......... .......... .......... .......... 69% 3.72M 11s
185250K .......... .......... .......... .......... .......... 69% 4.61M 11s
185300K .......... .......... .......... .......... .......... 69% 4.09M 11s
185350K .......... .......... .......... .......... .......... 69% 2.20M 11s
185400K .......... .......... .......... .......... .......... 69% 1.66M 11s
185450K .......... .......... .......... .......... .......... 69% 3.67M 11s
185500K .......... .......... .......... .......... .......... 69% 8.58M 11s
185550K .......... .......... .......... .......... .......... 69% 7.00M 11s
185600K .......... .......... .......... .......... .......... 69% 8.22M 11s
185650K .......... .......... .......... .......... .......... 69% 5.89M 11s
185700K .......... .......... .......... .......... .......... 69% 4.24M 11s
185750K .......... .......... .......... .......... .......... 69% 3.98M 11s
185800K .......... .......... .......... .......... .......... 69% 2.65M 11s
185850K .......... .......... .......... .......... .......... 69% 2.51M 11s
185900K .......... .......... .......... .......... .......... 69% 3.93M 11s
185950K .......... .......... .......... .......... .......... 69% 5.36M 11s
186000K .......... .......... .......... .......... .......... 70% 8.06M 11s
186050K .......... .......... .......... .......... .......... 70% 7.67M 11s
186100K .......... .......... .......... .......... .......... 70% 5.66M 11s
186150K .......... .......... .......... .......... .......... 70% 8.41M 11s
186200K .......... .......... .......... .......... .......... 70% 9.82M 11s
186250K .......... .......... .......... .......... .......... 70% 5.23M 11s
186300K .......... .......... .......... .......... .......... 70% 6.65M 11s
186350K .......... .......... .......... .......... .......... 70% 5.65M 11s
186400K .......... .......... .......... .......... .......... 70% 6.29M 11s
186450K .......... .......... .......... .......... .......... 70% 5.91M 11s
186500K .......... .......... .......... .......... .......... 70% 5.53M 11s
186550K .......... .......... .......... .......... .......... 70% 41.8M 11s
186600K .......... .......... .......... .......... .......... 70% 6.85M 11s
186650K .......... .......... .......... .......... .......... 70% 9.43M 11s
186700K .......... .......... .......... .......... .......... 70% 4.55M 11s
186750K .......... .......... .......... .......... .......... 70% 3.85M 11s
186800K .......... .......... .......... .......... .......... 70% 4.53M 11s
186850K .......... .......... .......... .......... .......... 70% 2.67M 11s
186900K .......... .......... .......... .......... .......... 70% 4.57M 11s
186950K .......... .......... .......... .......... .......... 70% 3.05M 11s
187000K .......... .......... .......... .......... .......... 70% 3.62M 11s
187050K .......... .......... .......... .......... .......... 70% 4.09M 11s
187100K .......... .......... .......... .......... .......... 70% 3.03M 11s
187150K .......... .......... .......... .......... .......... 70% 7.46M 11s
187200K .......... .......... .......... .......... .......... 70% 7.06M 11s
187250K .......... .......... .......... .......... .......... 70% 9.87M 11s
187300K .......... .......... .......... .......... .......... 70% 10.1M 11s
187350K .......... .......... .......... .......... .......... 70% 6.76M 11s
187400K .......... .......... .......... .......... .......... 70% 4.79M 11s
187450K .......... .......... .......... .......... .......... 70% 2.93M 11s
187500K .......... .......... .......... .......... .......... 70% 3.71M 11s
187550K .......... .......... .......... .......... .......... 70% 3.74M 11s
187600K .......... .......... .......... .......... .......... 70% 5.13M 11s
187650K .......... .......... .......... .......... .......... 70% 8.94M 11s
187700K .......... .......... .......... .......... .......... 70% 7.73M 11s
187750K .......... .......... .......... .......... .......... 70% 10.1M 11s
187800K .......... .......... .......... .......... .......... 70% 7.54M 11s
187850K .......... .......... .......... .......... .......... 70% 7.64M 11s
187900K .......... .......... .......... .......... .......... 70% 7.24M 11s
187950K .......... .......... .......... .......... .......... 70% 4.40M 11s
188000K .......... .......... .......... .......... .......... 70% 4.38M 11s
188050K .......... .......... .......... .......... .......... 70% 4.35M 11s
188100K .......... .......... .......... .......... .......... 70% 5.30M 11s
188150K .......... .......... .......... .......... .......... 70% 5.02M 11s
188200K .......... .......... .......... .......... .......... 70% 3.64M 11s
188250K .......... .......... .......... .......... .......... 70% 7.64M 11s
188300K .......... .......... .......... .......... .......... 70% 10.9M 11s
188350K .......... .......... .......... .......... .......... 70% 7.50M 11s
188400K .......... .......... .......... .......... .......... 70% 8.24M 11s
188450K .......... .......... .......... .......... .......... 70% 5.79M 11s
188500K .......... .......... .......... .......... .......... 70% 7.72M 11s
188550K .......... .......... .......... .......... .......... 70% 6.37M 11s
188600K .......... .......... .......... .......... .......... 70% 6.44M 11s
188650K .......... .......... .......... .......... .......... 70% 10.1M 11s
188700K .......... .......... .......... .......... .......... 71% 18.1M 11s
188750K .......... .......... .......... .......... .......... 71% 8.95M 11s
188800K .......... .......... .......... .......... .......... 71% 14.5M 11s
188850K .......... .......... .......... .......... .......... 71% 11.9M 11s
188900K .......... .......... .......... .......... .......... 71% 10.1M 11s
188950K .......... .......... .......... .......... .......... 71% 10.9M 11s
189000K .......... .......... .......... .......... .......... 71% 8.12M 11s
189050K .......... .......... .......... .......... .......... 71% 9.36M 11s
189100K .......... .......... .......... .......... .......... 71% 5.40M 11s
189150K .......... .......... .......... .......... .......... 71% 6.38M 11s
189200K .......... .......... .......... .......... .......... 71% 3.71M 11s
189250K .......... .......... .......... .......... .......... 71% 4.92M 11s
189300K .......... .......... .......... .......... .......... 71% 4.89M 11s
189350K .......... .......... .......... .......... .......... 71% 3.28M 11s
189400K .......... .......... .......... .......... .......... 71% 4.75M 11s
189450K .......... .......... .......... .......... .......... 71% 3.88M 11s
189500K .......... .......... .......... .......... .......... 71% 3.73M 11s
189550K .......... .......... .......... .......... .......... 71% 2.87M 11s
189600K .......... .......... .......... .......... .......... 71% 4.82M 11s
189650K .......... .......... .......... .......... .......... 71% 8.34M 11s
189700K .......... .......... .......... .......... .......... 71% 8.85M 11s
189750K .......... .......... .......... .......... .......... 71% 9.29M 11s
189800K .......... .......... .......... .......... .......... 71% 7.19M 11s
189850K .......... .......... .......... .......... .......... 71% 9.28M 11s
189900K .......... .......... .......... .......... .......... 71% 7.54M 11s
189950K .......... .......... .......... .......... .......... 71% 5.90M 11s
190000K .......... .......... .......... .......... .......... 71% 6.18M 11s
190050K .......... .......... .......... .......... .......... 71% 4.29M 10s
190100K .......... .......... .......... .......... .......... 71% 3.88M 10s
190150K .......... .......... .......... .......... .......... 71% 3.26M 10s
190200K .......... .......... .......... .......... .......... 71% 3.16M 10s
190250K .......... .......... .......... .......... .......... 71% 3.98M 10s
190300K .......... .......... .......... .......... .......... 71% 6.70M 10s
190350K .......... .......... .......... .......... .......... 71% 6.05M 10s
190400K .......... .......... .......... .......... .......... 71% 5.87M 10s
190450K .......... .......... .......... .......... .......... 71% 4.45M 10s
190500K .......... .......... .......... .......... .......... 71% 5.31M 10s
190550K .......... .......... .......... .......... .......... 71% 4.82M 10s
190600K .......... .......... .......... .......... .......... 71% 4.05M 10s
190650K .......... .......... .......... .......... .......... 71% 4.23M 10s
190700K .......... .......... .......... .......... .......... 71% 3.12M 10s
190750K .......... .......... .......... .......... .......... 71% 2.98M 10s
190800K .......... .......... .......... .......... .......... 71% 4.05M 10s
190850K .......... .......... .......... .......... .......... 71% 4.04M 10s
190900K .......... .......... .......... .......... .......... 71% 3.95M 10s
190950K .......... .......... .......... .......... .......... 71% 3.32M 10s
191000K .......... .......... .......... .......... .......... 71% 1.93M 10s
191050K .......... .......... .......... .......... .......... 71% 1.97M 10s
191100K .......... .......... .......... .......... .......... 71% 5.13M 10s
191150K .......... .......... .......... .......... .......... 71% 4.77M 10s
191200K .......... .......... .......... .......... .......... 71% 3.98M 10s
191250K .......... .......... .......... .......... .......... 71% 4.12M 10s
191300K .......... .......... .......... .......... .......... 71% 5.79M 10s
191350K .......... .......... .......... .......... .......... 72% 14.5M 10s
191400K .......... .......... .......... .......... .......... 72% 11.9M 10s
191450K .......... .......... .......... .......... .......... 72% 8.78M 10s
191500K .......... .......... .......... .......... .......... 72% 7.79M 10s
191550K .......... .......... .......... .......... .......... 72% 7.51M 10s
191600K .......... .......... .......... .......... .......... 72% 8.09M 10s
191650K .......... .......... .......... .......... .......... 72% 8.71M 10s
191700K .......... .......... .......... .......... .......... 72% 6.16M 10s
191750K .......... .......... .......... .......... .......... 72% 5.72M 10s
191800K .......... .......... .......... .......... .......... 72% 5.51M 10s
191850K .......... .......... .......... .......... .......... 72% 5.14M 10s
191900K .......... .......... .......... .......... .......... 72% 5.89M 10s
191950K .......... .......... .......... .......... .......... 72% 5.01M 10s
192000K .......... .......... .......... .......... .......... 72% 8.04M 10s
192050K .......... .......... .......... .......... .......... 72% 4.66M 10s
192100K .......... .......... .......... .......... .......... 72% 3.37M 10s
192150K .......... .......... .......... .......... .......... 72% 4.46M 10s
192200K .......... .......... .......... .......... .......... 72% 4.64M 10s
192250K .......... .......... .......... .......... .......... 72% 8.82M 10s
192300K .......... .......... .......... .......... .......... 72% 11.6M 10s
192350K .......... .......... .......... .......... .......... 72% 6.49M 10s
192400K .......... .......... .......... .......... .......... 72% 6.16M 10s
192450K .......... .......... .......... .......... .......... 72% 3.73M 10s
192500K .......... .......... .......... .......... .......... 72% 4.21M 10s
192550K .......... .......... .......... .......... .......... 72% 3.66M 10s
192600K .......... .......... .......... .......... .......... 72% 4.04M 10s
192650K .......... .......... .......... .......... .......... 72% 3.26M 10s
192700K .......... .......... .......... .......... .......... 72% 2.86M 10s
192750K .......... .......... .......... .......... .......... 72% 2.17M 10s
192800K .......... .......... .......... .......... .......... 72% 1.71M 10s
192850K .......... .......... .......... .......... .......... 72% 2.28M 10s
192900K .......... .......... .......... .......... .......... 72% 4.59M 10s
192950K .......... .......... .......... .......... .......... 72% 3.23M 10s
193000K .......... .......... .......... .......... .......... 72% 4.88M 10s
193050K .......... .......... .......... .......... .......... 72% 14.4M 10s
193100K .......... .......... .......... .......... .......... 72% 7.51M 10s
193150K .......... .......... .......... .......... .......... 72% 7.28M 10s
193200K .......... .......... .......... .......... .......... 72% 6.76M 10s
193250K .......... .......... .......... .......... .......... 72% 7.93M 10s
193300K .......... .......... .......... .......... .......... 72% 10.5M 10s
193350K .......... .......... .......... .......... .......... 72% 5.39M 10s
193400K .......... .......... .......... .......... .......... 72% 6.27M 10s
193450K .......... .......... .......... .......... .......... 72% 3.04M 10s
193500K .......... .......... .......... .......... .......... 72% 3.28M 10s
193550K .......... .......... .......... .......... .......... 72% 4.36M 10s
193600K .......... .......... .......... .......... .......... 72% 3.69M 10s
193650K .......... .......... .......... .......... .......... 72% 5.66M 10s
193700K .......... .......... .......... .......... .......... 72% 9.87M 10s
193750K .......... .......... .......... .......... .......... 72% 6.66M 10s
193800K .......... .......... .......... .......... .......... 72% 5.91M 10s
193850K .......... .......... .......... .......... .......... 72% 5.39M 10s
193900K .......... .......... .......... .......... .......... 72% 4.57M 10s
193950K .......... .......... .......... .......... .......... 72% 3.90M 10s
194000K .......... .......... .......... .......... .......... 73% 5.69M 10s
194050K .......... .......... .......... .......... .......... 73% 4.71M 10s
194100K .......... .......... .......... .......... .......... 73% 5.81M 10s
194150K .......... .......... .......... .......... .......... 73% 11.3M 10s
194200K .......... .......... .......... .......... .......... 73% 14.7M 10s
194250K .......... .......... .......... .......... .......... 73% 13.0M 10s
194300K .......... .......... .......... .......... .......... 73% 12.3M 10s
194350K .......... .......... .......... .......... .......... 73% 7.41M 10s
194400K .......... .......... .......... .......... .......... 73% 10.4M 10s
194450K .......... .......... .......... .......... .......... 73% 7.10M 10s
194500K .......... .......... .......... .......... .......... 73% 6.89M 10s
194550K .......... .......... .......... .......... .......... 73% 10.3M 10s
194600K .......... .......... .......... .......... .......... 73% 6.78M 10s
194650K .......... .......... .......... .......... .......... 73% 7.72M 10s
194700K .......... .......... .......... .......... .......... 73% 7.15M 10s
194750K .......... .......... .......... .......... .......... 73% 4.76M 10s
194800K .......... .......... .......... .......... .......... 73%  124M 10s
194850K .......... .......... .......... .......... .......... 73% 21.7M 10s
194900K .......... .......... .......... .......... .......... 73% 6.56M 10s
194950K .......... .......... .......... .......... .......... 73% 8.92M 10s
195000K .......... .......... .......... .......... .......... 73% 8.23M 10s
195050K .......... .......... .......... .......... .......... 73% 7.78M 10s
195100K .......... .......... .......... .......... .......... 73% 5.08M 10s
195150K .......... .......... .......... .......... .......... 73% 7.14M 10s
195200K .......... .......... .......... .......... .......... 73% 8.74M 10s
195250K .......... .......... .......... .......... .......... 73% 10.2M 10s
195300K .......... .......... .......... .......... .......... 73% 8.99M 10s
195350K .......... .......... .......... .......... .......... 73% 9.12M 10s
195400K .......... .......... .......... .......... .......... 73% 7.83M 10s
195450K .......... .......... .......... .......... .......... 73% 6.85M 10s
195500K .......... .......... .......... .......... .......... 73% 6.07M 10s
195550K .......... .......... .......... .......... .......... 73% 4.80M 10s
195600K .......... .......... .......... .......... .......... 73% 3.79M 10s
195650K .......... .......... .......... .......... .......... 73% 3.91M 10s
195700K .......... .......... .......... .......... .......... 73% 5.88M 10s
195750K .......... .......... .......... .......... .......... 73% 7.33M 10s
195800K .......... .......... .......... .......... .......... 73% 27.5M 10s
195850K .......... .......... .......... .......... .......... 73% 11.4M 10s
195900K .......... .......... .......... .......... .......... 73% 7.10M 10s
195950K .......... .......... .......... .......... .......... 73% 10.5M 10s
196000K .......... .......... .......... .......... .......... 73% 8.85M 10s
196050K .......... .......... .......... .......... .......... 73% 7.27M 10s
196100K .......... .......... .......... .......... .......... 73% 5.34M 10s
196150K .......... .......... .......... .......... .......... 73% 5.13M 10s
196200K .......... .......... .......... .......... .......... 73% 3.59M 10s
196250K .......... .......... .......... .......... .......... 73% 4.12M 10s
196300K .......... .......... .......... .......... .......... 73% 11.7M 10s
196350K .......... .......... .......... .......... .......... 73% 12.8M 10s
196400K .......... .......... .......... .......... .......... 73% 8.83M 10s
196450K .......... .......... .......... .......... .......... 73% 6.77M 10s
196500K .......... .......... .......... .......... .......... 73% 9.71M 10s
196550K .......... .......... .......... .......... .......... 73% 7.18M 10s
196600K .......... .......... .......... .......... .......... 73% 7.21M 10s
196650K .......... .......... .......... .......... .......... 74% 5.96M 10s
196700K .......... .......... .......... .......... .......... 74% 2.95M 10s
196750K .......... .......... .......... .......... .......... 74% 3.59M 10s
196800K .......... .......... .......... .......... .......... 74% 3.63M 10s
196850K .......... .......... .......... .......... .......... 74% 8.63M 10s
196900K .......... .......... .......... .......... .......... 74% 13.3M 10s
196950K .......... .......... .......... .......... .......... 74% 7.12M 10s
197000K .......... .......... .......... .......... .......... 74% 8.94M 10s
197050K .......... .......... .......... .......... .......... 74% 9.00M 10s
197100K .......... .......... .......... .......... .......... 74% 6.24M 10s
197150K .......... .......... .......... .......... .......... 74% 7.31M 10s
197200K .......... .......... .......... .......... .......... 74% 6.98M 10s
197250K .......... .......... .......... .......... .......... 74% 10.6M 10s
197300K .......... .......... .......... .......... .......... 74% 15.7M 10s
197350K .......... .......... .......... .......... .......... 74% 10.5M 10s
197400K .......... .......... .......... .......... .......... 74% 13.6M 10s
197450K .......... .......... .......... .......... .......... 74% 8.76M 10s
197500K .......... .......... .......... .......... .......... 74% 9.28M 10s
197550K .......... .......... .......... .......... .......... 74% 8.22M 10s
197600K .......... .......... .......... .......... .......... 74% 9.84M 10s
197650K .......... .......... .......... .......... .......... 74% 9.41M 10s
197700K .......... .......... .......... .......... .......... 74% 3.57M 10s
197750K .......... .......... .......... .......... .......... 74% 5.76M 10s
197800K .......... .......... .......... .......... .......... 74% 3.49M 10s
197850K .......... .......... .......... .......... .......... 74% 2.99M 10s
197900K .......... .......... .......... .......... .......... 74% 4.48M 10s
197950K .......... .......... .......... .......... .......... 74% 3.61M 10s
198000K .......... .......... .......... .......... .......... 74% 7.89M 10s
198050K .......... .......... .......... .......... .......... 74% 6.86M 9s
198100K .......... .......... .......... .......... .......... 74% 6.50M 9s
198150K .......... .......... .......... .......... .......... 74% 4.93M 9s
198200K .......... .......... .......... .......... .......... 74% 4.00M 9s
198250K .......... .......... .......... .......... .......... 74% 5.85M 9s
198300K .......... .......... .......... .......... .......... 74% 4.36M 9s
198350K .......... .......... .......... .......... .......... 74% 3.83M 9s
198400K .......... .......... .......... .......... .......... 74% 9.60M 9s
198450K .......... .......... .......... .......... .......... 74% 13.4M 9s
198500K .......... .......... .......... .......... .......... 74% 9.57M 9s
198550K .......... .......... .......... .......... .......... 74% 8.04M 9s
198600K .......... .......... .......... .......... .......... 74% 4.46M 9s
198650K .......... .......... .......... .......... .......... 74% 4.84M 9s
198700K .......... .......... .......... .......... .......... 74% 5.21M 9s
198750K .......... .......... .......... .......... .......... 74% 5.16M 9s
198800K .......... .......... .......... .......... .......... 74% 6.86M 9s
198850K .......... .......... .......... .......... .......... 74% 5.86M 9s
198900K .......... .......... .......... .......... .......... 74% 7.50M 9s
198950K .......... .......... .......... .......... .......... 74% 3.94M 9s
199000K .......... .......... .......... .......... .......... 74% 5.14M 9s
199050K .......... .......... .......... .......... .......... 74% 4.97M 9s
199100K .......... .......... .......... .......... .......... 74% 3.87M 9s
199150K .......... .......... .......... .......... .......... 74% 8.05M 9s
199200K .......... .......... .......... .......... .......... 74% 8.22M 9s
199250K .......... .......... .......... .......... .......... 74% 12.3M 9s
199300K .......... .......... .......... .......... .......... 75% 11.8M 9s
199350K .......... .......... .......... .......... .......... 75% 4.88M 9s
199400K .......... .......... .......... .......... .......... 75% 5.37M 9s
199450K .......... .......... .......... .......... .......... 75% 3.38M 9s
199500K .......... .......... .......... .......... .......... 75% 2.88M 9s
199550K .......... .......... .......... .......... .......... 75% 3.16M 9s
199600K .......... .......... .......... .......... .......... 75% 3.04M 9s
199650K .......... .......... .......... .......... .......... 75% 3.22M 9s
199700K .......... .......... .......... .......... .......... 75% 3.05M 9s
199750K .......... .......... .......... .......... .......... 75% 3.23M 9s
199800K .......... .......... .......... .......... .......... 75% 4.45M 9s
199850K .......... .......... .......... .......... .......... 75% 1.94M 9s
199900K .......... .......... .......... .......... .......... 75% 2.21M 9s
199950K .......... .......... .......... .......... .......... 75% 7.26M 9s
200000K .......... .......... .......... .......... .......... 75% 8.50M 9s
200050K .......... .......... .......... .......... .......... 75% 9.64M 9s
200100K .......... .......... .......... .......... .......... 75% 6.25M 9s
200150K .......... .......... .......... .......... .......... 75% 7.66M 9s
200200K .......... .......... .......... .......... .......... 75% 6.78M 9s
200250K .......... .......... .......... .......... .......... 75% 6.68M 9s
200300K .......... .......... .......... .......... .......... 75% 5.66M 9s
200350K .......... .......... .......... .......... .......... 75% 4.74M 9s
200400K .......... .......... .......... .......... .......... 75% 5.60M 9s
200450K .......... .......... .......... .......... .......... 75% 5.17M 9s
200500K .......... .......... .......... .......... .......... 75% 10.6M 9s
200550K .......... .......... .......... .......... .......... 75% 11.1M 9s
200600K .......... .......... .......... .......... .......... 75% 10.5M 9s
200650K .......... .......... .......... .......... .......... 75% 7.76M 9s
200700K .......... .......... .......... .......... .......... 75% 8.04M 9s
200750K .......... .......... .......... .......... .......... 75% 5.24M 9s
200800K .......... .......... .......... .......... .......... 75% 10.3M 9s
200850K .......... .......... .......... .......... .......... 75% 5.55M 9s
200900K .......... .......... .......... .......... .......... 75% 6.06M 9s
200950K .......... .......... .......... .......... .......... 75% 5.20M 9s
201000K .......... .......... .......... .......... .......... 75% 7.56M 9s
201050K .......... .......... .......... .......... .......... 75% 4.46M 9s
201100K .......... .......... .......... .......... .......... 75% 4.97M 9s
201150K .......... .......... .......... .......... .......... 75% 6.01M 9s
201200K .......... .......... .......... .......... .......... 75% 5.40M 9s
201250K .......... .......... .......... .......... .......... 75% 5.82M 9s
201300K .......... .......... .......... .......... .......... 75% 12.4M 9s
201350K .......... .......... .......... .......... .......... 75% 18.0M 9s
201400K .......... .......... .......... .......... .......... 75% 16.9M 9s
201450K .......... .......... .......... .......... .......... 75% 20.2M 9s
201500K .......... .......... .......... .......... .......... 75% 14.3M 9s
201550K .......... .......... .......... .......... .......... 75% 13.8M 9s
201600K .......... .......... .......... .......... .......... 75% 14.4M 9s
201650K .......... .......... .......... .......... .......... 75% 11.4M 9s
201700K .......... .......... .......... .......... .......... 75% 8.97M 9s
201750K .......... .......... .......... .......... .......... 75% 5.93M 9s
201800K .......... .......... .......... .......... .......... 75% 3.89M 9s
201850K .......... .......... .......... .......... .......... 75% 4.47M 9s
201900K .......... .......... .......... .......... .......... 75% 5.96M 9s
201950K .......... .......... .......... .......... .......... 76% 5.87M 9s
202000K .......... .......... .......... .......... .......... 76% 6.49M 9s
202050K .......... .......... .......... .......... .......... 76% 8.88M 9s
202100K .......... .......... .......... .......... .......... 76% 6.93M 9s
202150K .......... .......... .......... .......... .......... 76% 4.40M 9s
202200K .......... .......... .......... .......... .......... 76% 5.20M 9s
202250K .......... .......... .......... .......... .......... 76% 5.42M 9s
202300K .......... .......... .......... .......... .......... 76% 3.62M 9s
202350K .......... .......... .......... .......... .......... 76% 3.10M 9s
202400K .......... .......... .......... .......... .......... 76% 3.51M 9s
202450K .......... .......... .......... .......... .......... 76% 2.78M 9s
202500K .......... .......... .......... .......... .......... 76% 2.66M 9s
202550K .......... .......... .......... .......... .......... 76% 3.05M 9s
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202650K .......... .......... .......... .......... .......... 76% 1.36M 9s
202700K .......... .......... .......... .......... .......... 76% 2.03M 9s
202750K .......... .......... .......... .......... .......... 76% 11.8M 9s
202800K .......... .......... .......... .......... .......... 76% 13.0M 9s
202850K .......... .......... .......... .......... .......... 76% 19.8M 9s
202900K .......... .......... .......... .......... .......... 76% 16.6M 9s
202950K .......... .......... .......... .......... .......... 76% 14.0M 9s
203000K .......... .......... .......... .......... .......... 76% 10.3M 9s
203050K .......... .......... .......... .......... .......... 76% 22.7M 9s
203100K .......... .......... .......... .......... .......... 76% 7.72M 9s
203150K .......... .......... .......... .......... .......... 76% 7.65M 9s
203200K .......... .......... .......... .......... .......... 76% 5.30M 9s
203250K .......... .......... .......... .......... .......... 76% 7.35M 9s
203300K .......... .......... .......... .......... .......... 76% 7.73M 9s
203350K .......... .......... .......... .......... .......... 76% 3.87M 9s
203400K .......... .......... .......... .......... .......... 76% 4.15M 9s
203450K .......... .......... .......... .......... .......... 76% 2.64M 9s
203500K .......... .......... .......... .......... .......... 76% 4.00M 9s
203550K .......... .......... .......... .......... .......... 76% 7.10M 9s
203600K .......... .......... .......... .......... .......... 76% 9.74M 9s
203650K .......... .......... .......... .......... .......... 76% 6.00M 9s
203700K .......... .......... .......... .......... .......... 76% 6.90M 9s
203750K .......... .......... .......... .......... .......... 76% 7.95M 9s
203800K .......... .......... .......... .......... .......... 76% 7.79M 9s
203850K .......... .......... .......... .......... .......... 76% 5.77M 9s
203900K .......... .......... .......... .......... .......... 76% 4.14M 9s
203950K .......... .......... .......... .......... .......... 76% 4.37M 9s
204000K .......... .......... .......... .......... .......... 76% 5.65M 9s
204050K .......... .......... .......... .......... .......... 76% 5.79M 9s
204100K .......... .......... .......... .......... .......... 76% 5.53M 9s
204150K .......... .......... .......... .......... .......... 76% 6.46M 9s
204200K .......... .......... .......... .......... .......... 76% 6.39M 9s
204250K .......... .......... .......... .......... .......... 76% 8.84M 9s
204300K .......... .......... .......... .......... .......... 76% 28.5M 9s
204350K .......... .......... .......... .......... .......... 76% 19.4M 9s
204400K .......... .......... .......... .......... .......... 76% 20.9M 9s
204450K .......... .......... .......... .......... .......... 76% 12.2M 9s
204500K .......... .......... .......... .......... .......... 76% 84.0M 9s
204550K .......... .......... .......... .......... .......... 76% 9.16M 9s
204600K .......... .......... .......... .......... .......... 76% 10.1M 9s
204650K .......... .......... .......... .......... .......... 77% 6.98M 9s
204700K .......... .......... .......... .......... .......... 77% 5.90M 9s
204750K .......... .......... .......... .......... .......... 77% 7.59M 9s
204800K .......... .......... .......... .......... .......... 77% 8.45M 9s
204850K .......... .......... .......... .......... .......... 77% 7.42M 9s
204900K .......... .......... .......... .......... .......... 77% 8.74M 9s
204950K .......... .......... .......... .......... .......... 77% 5.45M 9s
205000K .......... .......... .......... .......... .......... 77% 8.80M 9s
205050K .......... .......... .......... .......... .......... 77% 6.59M 9s
205100K .......... .......... .......... .......... .......... 77% 2.83M 9s
205150K .......... .......... .......... .......... .......... 77% 4.19M 9s
205200K .......... .......... .......... .......... .......... 77% 4.14M 9s
205250K .......... .......... .......... .......... .......... 77% 17.6M 9s
205300K .......... .......... .......... .......... .......... 77% 19.3M 9s
205350K .......... .......... .......... .......... .......... 77% 11.4M 9s
205400K .......... .......... .......... .......... .......... 77% 17.0M 9s
205450K .......... .......... .......... .......... .......... 77% 11.9M 9s
205500K .......... .......... .......... .......... .......... 77% 11.2M 9s
205550K .......... .......... .......... .......... .......... 77% 5.94M 9s
205600K .......... .......... .......... .......... .......... 77% 5.91M 9s
205650K .......... .......... .......... .......... .......... 77% 6.16M 8s
205700K .......... .......... .......... .......... .......... 77% 4.09M 8s
205750K .......... .......... .......... .......... .......... 77% 4.78M 8s
205800K .......... .......... .......... .......... .......... 77% 4.65M 8s
205850K .......... .......... .......... .......... .......... 77% 3.55M 8s
205900K .......... .......... .......... .......... .......... 77% 5.13M 8s
205950K .......... .......... .......... .......... .......... 77% 3.81M 8s
206000K .......... .......... .......... .......... .......... 77% 4.75M 8s
206050K .......... .......... .......... .......... .......... 77% 4.12M 8s
206100K .......... .......... .......... .......... .......... 77% 4.28M 8s
206150K .......... .......... .......... .......... .......... 77% 4.98M 8s
206200K .......... .......... .......... .......... .......... 77% 4.69M 8s
206250K .......... .......... .......... .......... .......... 77% 11.4M 8s
206300K .......... .......... .......... .......... .......... 77% 27.6M 8s
206350K .......... .......... .......... .......... .......... 77% 21.5M 8s
206400K .......... .......... .......... .......... .......... 77% 16.7M 8s
206450K .......... .......... .......... .......... .......... 77% 28.8M 8s
206500K .......... .......... .......... .......... .......... 77% 15.2M 8s
206550K .......... .......... .......... .......... .......... 77% 15.6M 8s
206600K .......... .......... .......... .......... .......... 77% 7.77M 8s
206650K .......... .......... .......... .......... .......... 77% 12.1M 8s
206700K .......... .......... .......... .......... .......... 77% 11.2M 8s
206750K .......... .......... .......... .......... .......... 77% 8.27M 8s
206800K .......... .......... .......... .......... .......... 77% 8.57M 8s
206850K .......... .......... .......... .......... .......... 77% 4.39M 8s
206900K .......... .......... .......... .......... .......... 77% 4.83M 8s
206950K .......... .......... .......... .......... .......... 77% 3.73M 8s
207000K .......... .......... .......... .......... .......... 77% 3.73M 8s
207050K .......... .......... .......... .......... .......... 77% 3.85M 8s
207100K .......... .......... .......... .......... .......... 77% 4.26M 8s
207150K .......... .......... .......... .......... .......... 77% 10.1M 8s
207200K .......... .......... .......... .......... .......... 77% 10.5M 8s
207250K .......... .......... .......... .......... .......... 77% 14.1M 8s
207300K .......... .......... .......... .......... .......... 78% 8.07M 8s
207350K .......... .......... .......... .......... .......... 78% 7.14M 8s
207400K .......... .......... .......... .......... .......... 78% 9.68M 8s
207450K .......... .......... .......... .......... .......... 78% 8.10M 8s
207500K .......... .......... .......... .......... .......... 78% 6.25M 8s
207550K .......... .......... .......... .......... .......... 78% 4.76M 8s
207600K .......... .......... .......... .......... .......... 78% 4.38M 8s
207650K .......... .......... .......... .......... .......... 78% 4.71M 8s
207700K .......... .......... .......... .......... .......... 78% 4.02M 8s
207750K .......... .......... .......... .......... .......... 78% 5.08M 8s
207800K .......... .......... .......... .......... .......... 78% 4.60M 8s
207850K .......... .......... .......... .......... .......... 78% 4.54M 8s
207900K .......... .......... .......... .......... .......... 78% 18.5M 8s
207950K .......... .......... .......... .......... .......... 78% 9.79M 8s
208000K .......... .......... .......... .......... .......... 78% 21.6M 8s
208050K .......... .......... .......... .......... .......... 78% 14.0M 8s
208100K .......... .......... .......... .......... .......... 78% 10.6M 8s
208150K .......... .......... .......... .......... .......... 78% 12.6M 8s
208200K .......... .......... .......... .......... .......... 78% 6.07M 8s
208250K .......... .......... .......... .......... .......... 78% 10.5M 8s
208300K .......... .......... .......... .......... .......... 78% 6.61M 8s
208350K .......... .......... .......... .......... .......... 78% 4.63M 8s
208400K .......... .......... .......... .......... .......... 78% 6.96M 8s
208450K .......... .......... .......... .......... .......... 78% 3.15M 8s
208500K .......... .......... .......... .......... .......... 78% 2.46M 8s
208550K .......... .......... .......... .......... .......... 78% 3.52M 8s
208600K .......... .......... .......... .......... .......... 78% 12.6M 8s
208650K .......... .......... .......... .......... .......... 78% 11.4M 8s
208700K .......... .......... .......... .......... .......... 78% 7.48M 8s
208750K .......... .......... .......... .......... .......... 78% 10.5M 8s
208800K .......... .......... .......... .......... .......... 78% 9.12M 8s
208850K .......... .......... .......... .......... .......... 78% 8.37M 8s
208900K .......... .......... .......... .......... .......... 78% 8.52M 8s
208950K .......... .......... .......... .......... .......... 78% 7.88M 8s
209000K .......... .......... .......... .......... .......... 78% 11.3M 8s
209050K .......... .......... .......... .......... .......... 78% 11.0M 8s
209100K .......... .......... .......... .......... .......... 78% 8.81M 8s
209150K .......... .......... .......... .......... .......... 78% 9.30M 8s
209200K .......... .......... .......... .......... .......... 78% 10.8M 8s
209250K .......... .......... .......... .......... .......... 78%  103M 8s
209300K .......... .......... .......... .......... .......... 78% 27.1M 8s
209350K .......... .......... .......... .......... .......... 78% 14.6M 8s
209400K .......... .......... .......... .......... .......... 78% 21.0M 8s
209450K .......... .......... .......... .......... .......... 78% 9.81M 8s
209500K .......... .......... .......... .......... .......... 78% 12.5M 8s
209550K .......... .......... .......... .......... .......... 78% 17.9M 8s
209600K .......... .......... .......... .......... .......... 78% 9.63M 8s
209650K .......... .......... .......... .......... .......... 78% 12.7M 8s
209700K .......... .......... .......... .......... .......... 78% 9.12M 8s
209750K .......... .......... .......... .......... .......... 78% 9.75M 8s
209800K .......... .......... .......... .......... .......... 78% 12.4M 8s
209850K .......... .......... .......... .......... .......... 78% 10.3M 8s
209900K .......... .......... .......... .......... .......... 78% 12.8M 8s
209950K .......... .......... .......... .......... .......... 79% 20.9M 8s
210000K .......... .......... .......... .......... .......... 79% 32.1M 8s
210050K .......... .......... .......... .......... .......... 79% 32.8M 8s
210100K .......... .......... .......... .......... .......... 79% 29.1M 8s
210150K .......... .......... .......... .......... .......... 79% 28.6M 8s
210200K .......... .......... .......... .......... .......... 79% 24.7M 8s
210250K .......... .......... .......... .......... .......... 79% 28.2M 8s
210300K .......... .......... .......... .......... .......... 79% 28.4M 8s
210350K .......... .......... .......... .......... .......... 79% 17.8M 8s
210400K .......... .......... .......... .......... .......... 79% 36.6M 8s
210450K .......... .......... .......... .......... .......... 79% 13.6M 8s
210500K .......... .......... .......... .......... .......... 79% 11.5M 8s
210550K .......... .......... .......... .......... .......... 79% 16.6M 8s
210600K .......... .......... .......... .......... .......... 79% 6.62M 8s
210650K .......... .......... .......... .......... .......... 79% 6.34M 8s
210700K .......... .......... .......... .......... .......... 79% 4.62M 8s
210750K .......... .......... .......... .......... .......... 79% 5.68M 8s
210800K .......... .......... .......... .......... .......... 79% 5.64M 8s
210850K .......... .......... .......... .......... .......... 79% 4.81M 8s
210900K .......... .......... .......... .......... .......... 79% 4.36M 8s
210950K .......... .......... .......... .......... .......... 79% 3.54M 8s
211000K .......... .......... .......... .......... .......... 79% 2.96M 8s
211050K .......... .......... .......... .......... .......... 79% 2.27M 8s
211100K .......... .......... .......... .......... .......... 79% 2.49M 8s
211150K .......... .......... .......... .......... .......... 79% 9.45M 8s
211200K .......... .......... .......... .......... .......... 79% 9.24M 8s
211250K .......... .......... .......... .......... .......... 79% 9.46M 8s
211300K .......... .......... .......... .......... .......... 79% 9.55M 8s
211350K .......... .......... .......... .......... .......... 79% 7.59M 8s
211400K .......... .......... .......... .......... .......... 79% 7.34M 8s
211450K .......... .......... .......... .......... .......... 79% 5.95M 8s
211500K .......... .......... .......... .......... .......... 79% 7.92M 8s
211550K .......... .......... .......... .......... .......... 79% 7.56M 8s
211600K .......... .......... .......... .......... .......... 79% 5.59M 8s
211650K .......... .......... .......... .......... .......... 79% 8.83M 8s
211700K .......... .......... .......... .......... .......... 79% 13.6M 8s
211750K .......... .......... .......... .......... .......... 79% 13.9M 8s
211800K .......... .......... .......... .......... .......... 79% 13.9M 8s
211850K .......... .......... .......... .......... .......... 79% 14.0M 8s
211900K .......... .......... .......... .......... .......... 79% 15.3M 8s
211950K .......... .......... .......... .......... .......... 79% 15.3M 8s
212000K .......... .......... .......... .......... .......... 79% 9.77M 8s
212050K .......... .......... .......... .......... .......... 79% 8.18M 8s
212100K .......... .......... .......... .......... .......... 79% 8.25M 8s
212150K .......... .......... .......... .......... .......... 79% 8.29M 8s
212200K .......... .......... .......... .......... .......... 79% 7.41M 8s
212250K .......... .......... .......... .......... .......... 79% 9.48M 8s
212300K .......... .......... .......... .......... .......... 79% 9.50M 8s
212350K .......... .......... .......... .......... .......... 79% 8.08M 8s
212400K .......... .......... .......... .......... .......... 79% 6.80M 8s
212450K .......... .......... .......... .......... .......... 79% 6.91M 8s
212500K .......... .......... .......... .......... .......... 79% 7.70M 8s
212550K .......... .......... .......... .......... .......... 79% 7.47M 8s
212600K .......... .......... .......... .......... .......... 80% 3.82M 7s
212650K .......... .......... .......... .......... .......... 80% 3.81M 7s
212700K .......... .......... .......... .......... .......... 80% 2.60M 7s
212750K .......... .......... .......... .......... .......... 80% 2.26M 7s
212800K .......... .......... .......... .......... .......... 80% 2.34M 7s
212850K .......... .......... .......... .......... .......... 80% 2.03M 7s
212900K .......... .......... .......... .......... .......... 80% 6.59M 7s
212950K .......... .......... .......... .......... .......... 80% 3.76M 7s
213000K .......... .......... .......... .......... .......... 80% 4.56M 7s
213050K .......... .......... .......... .......... .......... 80% 3.76M 7s
213100K .......... .......... .......... .......... .......... 80% 4.59M 7s
213150K .......... .......... .......... .......... .......... 80% 5.47M 7s
213200K .......... .......... .......... .......... .......... 80% 3.93M 7s
213250K .......... .......... .......... .......... .......... 80% 3.75M 7s
213300K .......... .......... .......... .......... .......... 80% 4.19M 7s
213350K .......... .......... .......... .......... .......... 80% 5.26M 7s
213400K .......... .......... .......... .......... .......... 80% 6.34M 7s
213450K .......... .......... .......... .......... .......... 80% 5.90M 7s
213500K .......... .......... .......... .......... .......... 80% 8.47M 7s
213550K .......... .......... .......... .......... .......... 80% 7.86M 7s
213600K .......... .......... .......... .......... .......... 80% 18.1M 7s
213650K .......... .......... .......... .......... .......... 80% 28.7M 7s
213700K .......... .......... .......... .......... .......... 80% 12.1M 7s
213750K .......... .......... .......... .......... .......... 80% 28.5M 7s
213800K .......... .......... .......... .......... .......... 80% 16.0M 7s
213850K .......... .......... .......... .......... .......... 80% 18.6M 7s
213900K .......... .......... .......... .......... .......... 80% 17.3M 7s
213950K .......... .......... .......... .......... .......... 80% 16.7M 7s
214000K .......... .......... .......... .......... .......... 80% 21.0M 7s
214050K .......... .......... .......... .......... .......... 80% 18.0M 7s
214100K .......... .......... .......... .......... .......... 80% 13.3M 7s
214150K .......... .......... .......... .......... .......... 80% 21.8M 7s
214200K .......... .......... .......... .......... .......... 80% 10.3M 7s
214250K .......... .......... .......... .......... .......... 80% 12.4M 7s
214300K .......... .......... .......... .......... .......... 80% 15.5M 7s
214350K .......... .......... .......... .......... .......... 80% 8.58M 7s
214400K .......... .......... .......... .......... .......... 80% 8.14M 7s
214450K .......... .......... .......... .......... .......... 80% 4.83M 7s
214500K .......... .......... .......... .......... .......... 80% 7.06M 7s
214550K .......... .......... .......... .......... .......... 80% 6.41M 7s
214600K .......... .......... .......... .......... .......... 80% 5.59M 7s
214650K .......... .......... .......... .......... .......... 80% 7.21M 7s
214700K .......... .......... .......... .......... .......... 80% 7.35M 7s
214750K .......... .......... .......... .......... .......... 80% 14.8M 7s
214800K .......... .......... .......... .......... .......... 80% 16.8M 7s
214850K .......... .......... .......... .......... .......... 80% 12.0M 7s
214900K .......... .......... .......... .......... .......... 80% 9.15M 7s
214950K .......... .......... .......... .......... .......... 80% 12.2M 7s
215000K .......... .......... .......... .......... .......... 80% 14.7M 7s
215050K .......... .......... .......... .......... .......... 80% 10.6M 7s
215100K .......... .......... .......... .......... .......... 80% 10.8M 7s
215150K .......... .......... .......... .......... .......... 80% 13.1M 7s
215200K .......... .......... .......... .......... .......... 80% 7.83M 7s
215250K .......... .......... .......... .......... .......... 81% 10.5M 7s
215300K .......... .......... .......... .......... .......... 81% 8.93M 7s
215350K .......... .......... .......... .......... .......... 81% 10.3M 7s
215400K .......... .......... .......... .......... .......... 81% 15.3M 7s
215450K .......... .......... .......... .......... .......... 81% 10.1M 7s
215500K .......... .......... .......... .......... .......... 81% 5.71M 7s
215550K .......... .......... .......... .......... .......... 81%  116M 7s
215600K .......... .......... .......... .......... .......... 81% 11.7M 7s
215650K .......... .......... .......... .......... .......... 81% 11.2M 7s
215700K .......... .......... .......... .......... .......... 81% 5.44M 7s
215750K .......... .......... .......... .......... .......... 81% 13.3M 7s
215800K .......... .......... .......... .......... .......... 81% 6.65M 7s
215850K .......... .......... .......... .......... .......... 81% 6.98M 7s
215900K .......... .......... .......... .......... .......... 81% 9.34M 7s
215950K .......... .......... .......... .......... .......... 81% 5.58M 7s
216000K .......... .......... .......... .......... .......... 81% 5.43M 7s
216050K .......... .......... .......... .......... .......... 81% 5.44M 7s
216100K .......... .......... .......... .......... .......... 81% 4.37M 7s
216150K .......... .......... .......... .......... .......... 81% 4.59M 7s
216200K .......... .......... .......... .......... .......... 81% 6.81M 7s
216250K .......... .......... .......... .......... .......... 81% 9.24M 7s
216300K .......... .......... .......... .......... .......... 81% 11.1M 7s
216350K .......... .......... .......... .......... .......... 81% 8.57M 7s
216400K .......... .......... .......... .......... .......... 81% 8.39M 7s
216450K .......... .......... .......... .......... .......... 81% 6.27M 7s
216500K .......... .......... .......... .......... .......... 81% 7.28M 7s
216550K .......... .......... .......... .......... .......... 81% 6.42M 7s
216600K .......... .......... .......... .......... .......... 81% 5.42M 7s
216650K .......... .......... .......... .......... .......... 81% 6.65M 7s
216700K .......... .......... .......... .......... .......... 81% 4.65M 7s
216750K .......... .......... .......... .......... .......... 81% 6.31M 7s
216800K .......... .......... .......... .......... .......... 81% 6.14M 7s
216850K .......... .......... .......... .......... .......... 81% 4.36M 7s
216900K .......... .......... .......... .......... .......... 81% 5.06M 7s
216950K .......... .......... .......... .......... .......... 81% 3.08M 7s
217000K .......... .......... .......... .......... .......... 81% 4.18M 7s
217050K .......... .......... .......... .......... .......... 81% 4.15M 7s
217100K .......... .......... .......... .......... .......... 81% 8.81M 7s
217150K .......... .......... .......... .......... .......... 81% 12.0M 7s
217200K .......... .......... .......... .......... .......... 81% 27.2M 7s
217250K .......... .......... .......... .......... .......... 81% 15.5M 7s
217300K .......... .......... .......... .......... .......... 81% 6.93M 7s
217350K .......... .......... .......... .......... .......... 81% 5.18M 7s
217400K .......... .......... .......... .......... .......... 81% 8.03M 7s
217450K .......... .......... .......... .......... .......... 81% 7.99M 7s
217500K .......... .......... .......... .......... .......... 81% 8.12M 7s
217550K .......... .......... .......... .......... .......... 81% 5.37M 7s
217600K .......... .......... .......... .......... .......... 81% 6.83M 7s
217650K .......... .......... .......... .......... .......... 81% 10.1M 7s
217700K .......... .......... .......... .......... .......... 81% 7.20M 7s
217750K .......... .......... .......... .......... .......... 81% 9.17M 7s
217800K .......... .......... .......... .......... .......... 81% 10.2M 7s
217850K .......... .......... .......... .......... .......... 81% 6.06M 7s
217900K .......... .......... .......... .......... .......... 82% 6.12M 7s
217950K .......... .......... .......... .......... .......... 82% 3.81M 7s
218000K .......... .......... .......... .......... .......... 82% 5.19M 7s
218050K .......... .......... .......... .......... .......... 82% 4.53M 7s
218100K .......... .......... .......... .......... .......... 82% 4.82M 7s
218150K .......... .......... .......... .......... .......... 82% 4.22M 7s
218200K .......... .......... .......... .......... .......... 82% 3.87M 7s
218250K .......... .......... .......... .......... .......... 82% 4.18M 7s
218300K .......... .......... .......... .......... .......... 82% 5.45M 7s
218350K .......... .......... .......... .......... .......... 82% 3.20M 7s
218400K .......... .......... .......... .......... .......... 82% 2.87M 7s
218450K .......... .......... .......... .......... .......... 82% 1.85M 7s
218500K .......... .......... .......... .......... .......... 82% 1.20M 7s
218550K .......... .......... .......... .......... .......... 82% 2.75M 7s
218600K .......... .......... .......... .......... .......... 82% 2.31M 7s
218650K .......... .......... .......... .......... .......... 82% 2.91M 7s
218700K .......... .......... .......... .......... .......... 82% 2.02M 7s
218750K .......... .......... .......... .......... .......... 82% 2.50M 7s
218800K .......... .......... .......... .......... .......... 82% 3.39M 7s
218850K .......... .......... .......... .......... .......... 82% 2.74M 7s
218900K .......... .......... .......... .......... .......... 82% 8.71M 7s
218950K .......... .......... .......... .......... .......... 82% 10.5M 7s
219000K .......... .......... .......... .......... .......... 82% 9.80M 7s
219050K .......... .......... .......... .......... .......... 82% 6.42M 7s
219100K .......... .......... .......... .......... .......... 82% 4.13M 7s
219150K .......... .......... .......... .......... .......... 82% 6.41M 7s
219200K .......... .......... .......... .......... .......... 82% 5.66M 7s
219250K .......... .......... .......... .......... .......... 82% 7.30M 7s
219300K .......... .......... .......... .......... .......... 82% 14.7M 7s
219350K .......... .......... .......... .......... .......... 82% 21.0M 7s
219400K .......... .......... .......... .......... .......... 82% 30.0M 7s
219450K .......... .......... .......... .......... .......... 82% 9.10M 7s
219500K .......... .......... .......... .......... .......... 82%  150M 7s
219550K .......... .......... .......... .......... .......... 82% 33.9M 7s
219600K .......... .......... .......... .......... .......... 82% 13.3M 7s
219650K .......... .......... .......... .......... .......... 82% 9.69M 7s
219700K .......... .......... .......... .......... .......... 82% 18.1M 7s
219750K .......... .......... .......... .......... .......... 82% 11.4M 7s
219800K .......... .......... .......... .......... .......... 82% 7.97M 7s
219850K .......... .......... .......... .......... .......... 82% 9.16M 7s
219900K .......... .......... .......... .......... .......... 82% 7.02M 7s
219950K .......... .......... .......... .......... .......... 82% 6.47M 6s
220000K .......... .......... .......... .......... .......... 82% 5.00M 6s
220050K .......... .......... .......... .......... .......... 82% 5.10M 6s
220100K .......... .......... .......... .......... .......... 82% 5.07M 6s
220150K .......... .......... .......... .......... .......... 82% 6.53M 6s
220200K .......... .......... .......... .......... .......... 82% 4.50M 6s
220250K .......... .......... .......... .......... .......... 82% 5.71M 6s
220300K .......... .......... .......... .......... .......... 82% 5.07M 6s
220350K .......... .......... .......... .......... .......... 82% 4.94M 6s
220400K .......... .......... .......... .......... .......... 82% 6.20M 6s
220450K .......... .......... .......... .......... .......... 82% 7.50M 6s
220500K .......... .......... .......... .......... .......... 82% 20.5M 6s
220550K .......... .......... .......... .......... .......... 83% 17.4M 6s
220600K .......... .......... .......... .......... .......... 83% 30.6M 6s
220650K .......... .......... .......... .......... .......... 83% 15.7M 6s
220700K .......... .......... .......... .......... .......... 83% 15.2M 6s
220750K .......... .......... .......... .......... .......... 83% 16.2M 6s
220800K .......... .......... .......... .......... .......... 83% 16.5M 6s
220850K .......... .......... .......... .......... .......... 83% 10.3M 6s
220900K .......... .......... .......... .......... .......... 83% 9.56M 6s
220950K .......... .......... .......... .......... .......... 83% 6.08M 6s
221000K .......... .......... .......... .......... .......... 83% 5.74M 6s
221050K .......... .......... .......... .......... .......... 83% 5.29M 6s
221100K .......... .......... .......... .......... .......... 83% 4.33M 6s
221150K .......... .......... .......... .......... .......... 83% 4.75M 6s
221200K .......... .......... .......... .......... .......... 83% 3.46M 6s
221250K .......... .......... .......... .......... .......... 83% 7.90M 6s
221300K .......... .......... .......... .......... .......... 83% 9.66M 6s
221350K .......... .......... .......... .......... .......... 83% 5.85M 6s
221400K .......... .......... .......... .......... .......... 83% 10.5M 6s
221450K .......... .......... .......... .......... .......... 83% 10.2M 6s
221500K .......... .......... .......... .......... .......... 83% 10.0M 6s
221550K .......... .......... .......... .......... .......... 83% 5.42M 6s
221600K .......... .......... .......... .......... .......... 83% 5.72M 6s
221650K .......... .......... .......... .......... .......... 83% 5.94M 6s
221700K .......... .......... .......... .......... .......... 83% 5.42M 6s
221750K .......... .......... .......... .......... .......... 83% 21.0M 6s
221800K .......... .......... .......... .......... .......... 83% 25.9M 6s
221850K .......... .......... .......... .......... .......... 83% 26.9M 6s
221900K .......... .......... .......... .......... .......... 83% 35.1M 6s
221950K .......... .......... .......... .......... .......... 83% 15.1M 6s
222000K .......... .......... .......... .......... .......... 83% 72.3M 6s
222050K .......... .......... .......... .......... .......... 83% 19.8M 6s
222100K .......... .......... .......... .......... .......... 83% 19.2M 6s
222150K .......... .......... .......... .......... .......... 83% 23.9M 6s
222200K .......... .......... .......... .......... .......... 83% 18.1M 6s
222250K .......... .......... .......... .......... .......... 83% 17.8M 6s
222300K .......... .......... .......... .......... .......... 83% 33.7M 6s
222350K .......... .......... .......... .......... .......... 83% 12.1M 6s
222400K .......... .......... .......... .......... .......... 83% 14.4M 6s
222450K .......... .......... .......... .......... .......... 83% 8.25M 6s
222500K .......... .......... .......... .......... .......... 83% 9.27M 6s
222550K .......... .......... .......... .......... .......... 83% 8.77M 6s
222600K .......... .......... .......... .......... .......... 83% 6.79M 6s
222650K .......... .......... .......... .......... .......... 83% 7.39M 6s
222700K .......... .......... .......... .......... .......... 83% 7.89M 6s
222750K .......... .......... .......... .......... .......... 83% 14.4M 6s
222800K .......... .......... .......... .......... .......... 83% 72.7M 6s
222850K .......... .......... .......... .......... .......... 83% 13.9M 6s
222900K .......... .......... .......... .......... .......... 83% 16.7M 6s
222950K .......... .......... .......... .......... .......... 83% 9.00M 6s
223000K .......... .......... .......... .......... .......... 83% 10.7M 6s
223050K .......... .......... .......... .......... .......... 83% 10.9M 6s
223100K .......... .......... .......... .......... .......... 83% 6.92M 6s
223150K .......... .......... .......... .......... .......... 83% 15.6M 6s
223200K .......... .......... .......... .......... .......... 83% 6.07M 6s
223250K .......... .......... .......... .......... .......... 84% 4.85M 6s
223300K .......... .......... .......... .......... .......... 84% 6.07M 6s
223350K .......... .......... .......... .......... .......... 84% 5.13M 6s
223400K .......... .......... .......... .......... .......... 84% 5.37M 6s
223450K .......... .......... .......... .......... .......... 84% 5.35M 6s
223500K .......... .......... .......... .......... .......... 84% 7.11M 6s
223550K .......... .......... .......... .......... .......... 84% 14.2M 6s
223600K .......... .......... .......... .......... .......... 84% 16.1M 6s
223650K .......... .......... .......... .......... .......... 84% 24.7M 6s
223700K .......... .......... .......... .......... .......... 84% 13.8M 6s
223750K .......... .......... .......... .......... .......... 84% 12.7M 6s
223800K .......... .......... .......... .......... .......... 84% 15.1M 6s
223850K .......... .......... .......... .......... .......... 84% 16.5M 6s
223900K .......... .......... .......... .......... .......... 84% 12.5M 6s
223950K .......... .......... .......... .......... .......... 84% 16.1M 6s
224000K .......... .......... .......... .......... .......... 84% 19.3M 6s
224050K .......... .......... .......... .......... .......... 84% 24.5M 6s
224100K .......... .......... .......... .......... .......... 84% 14.7M 6s
224150K .......... .......... .......... .......... .......... 84% 22.8M 6s
224200K .......... .......... .......... .......... .......... 84% 16.5M 6s
224250K .......... .......... .......... .......... .......... 84% 14.8M 6s
224300K .......... .......... .......... .......... .......... 84% 15.4M 6s
224350K .......... .......... .......... .......... .......... 84% 12.6M 6s
224400K .......... .......... .......... .......... .......... 84% 12.0M 6s
224450K .......... .......... .......... .......... .......... 84% 12.8M 6s
224500K .......... .......... .......... .......... .......... 84% 9.73M 6s
224550K .......... .......... .......... .......... .......... 84% 6.94M 6s
224600K .......... .......... .......... .......... .......... 84% 5.90M 6s
224650K .......... .......... .......... .......... .......... 84% 8.84M 6s
224700K .......... .......... .......... .......... .......... 84% 6.41M 6s
224750K .......... .......... .......... .......... .......... 84% 7.94M 6s
224800K .......... .......... .......... .......... .......... 84% 10.5M 6s
224850K .......... .......... .......... .......... .......... 84% 19.1M 6s
224900K .......... .......... .......... .......... .......... 84% 19.9M 6s
224950K .......... .......... .......... .......... .......... 84% 17.5M 6s
225000K .......... .......... .......... .......... .......... 84% 18.8M 6s
225050K .......... .......... .......... .......... .......... 84% 12.0M 6s
225100K .......... .......... .......... .......... .......... 84% 18.3M 6s
225150K .......... .......... .......... .......... .......... 84% 10.6M 6s
225200K .......... .......... .......... .......... .......... 84% 10.1M 6s
225250K .......... .......... .......... .......... .......... 84% 11.3M 6s
225300K .......... .......... .......... .......... .......... 84% 10.3M 6s
225350K .......... .......... .......... .......... .......... 84% 8.35M 6s
225400K .......... .......... .......... .......... .......... 84% 10.0M 6s
225450K .......... .......... .......... .......... .......... 84% 9.04M 6s
225500K .......... .......... .......... .......... .......... 84% 12.8M 6s
225550K .......... .......... .......... .......... .......... 84% 11.3M 6s
225600K .......... .......... .......... .......... .......... 84% 7.16M 6s
225650K .......... .......... .......... .......... .......... 84% 7.50M 6s
225700K .......... .......... .......... .......... .......... 84% 12.4M 6s
225750K .......... .......... .......... .......... .......... 84% 12.0M 6s
225800K .......... .......... .......... .......... .......... 84% 8.17M 6s
225850K .......... .......... .......... .......... .......... 84% 17.7M 6s
225900K .......... .......... .......... .......... .......... 85% 10.3M 6s
225950K .......... .......... .......... .......... .......... 85% 11.5M 6s
226000K .......... .......... .......... .......... .......... 85% 11.7M 6s
226050K .......... .......... .......... .......... .......... 85% 10.3M 6s
226100K .......... .......... .......... .......... .......... 85% 12.4M 6s
226150K .......... .......... .......... .......... .......... 85% 11.1M 6s
226200K .......... .......... .......... .......... .......... 85% 11.9M 6s
226250K .......... .......... .......... .......... .......... 85% 12.7M 6s
226300K .......... .......... .......... .......... .......... 85% 14.4M 6s
226350K .......... .......... .......... .......... .......... 85% 10.7M 6s
226400K .......... .......... .......... .......... .......... 85% 9.53M 6s
226450K .......... .......... .......... .......... .......... 85% 11.4M 6s
226500K .......... .......... .......... .......... .......... 85% 13.8M 6s
226550K .......... .......... .......... .......... .......... 85% 16.1M 6s
226600K .......... .......... .......... .......... .......... 85% 10.0M 6s
226650K .......... .......... .......... .......... .......... 85% 12.1M 5s
226700K .......... .......... .......... .......... .......... 85% 9.00M 5s
226750K .......... .......... .......... .......... .......... 85% 10.5M 5s
226800K .......... .......... .......... .......... .......... 85% 9.80M 5s
226850K .......... .......... .......... .......... .......... 85% 9.63M 5s
226900K .......... .......... .......... .......... .......... 85% 11.0M 5s
226950K .......... .......... .......... .......... .......... 85% 10.1M 5s
227000K .......... .......... .......... .......... .......... 85% 14.2M 5s
227050K .......... .......... .......... .......... .......... 85% 20.5M 5s
227100K .......... .......... .......... .......... .......... 85% 14.8M 5s
227150K .......... .......... .......... .......... .......... 85% 16.5M 5s
227200K .......... .......... .......... .......... .......... 85% 16.8M 5s
227250K .......... .......... .......... .......... .......... 85% 15.6M 5s
227300K .......... .......... .......... .......... .......... 85% 16.1M 5s
227350K .......... .......... .......... .......... .......... 85% 16.4M 5s
227400K .......... .......... .......... .......... .......... 85% 34.8M 5s
227450K .......... .......... .......... .......... .......... 85%  116M 5s
227500K .......... .......... .......... .......... .......... 85% 44.1M 5s
227550K .......... .......... .......... .......... .......... 85% 31.4M 5s
227600K .......... .......... .......... .......... .......... 85% 38.3M 5s
227650K .......... .......... .......... .......... .......... 85% 33.2M 5s
227700K .......... .......... .......... .......... .......... 85% 35.1M 5s
227750K .......... .......... .......... .......... .......... 85% 33.8M 5s
227800K .......... .......... .......... .......... .......... 85% 42.0M 5s
227850K .......... .......... .......... .......... .......... 85% 26.0M 5s
227900K .......... .......... .......... .......... .......... 85% 34.6M 5s
227950K .......... .......... .......... .......... .......... 85% 26.6M 5s
228000K .......... .......... .......... .......... .......... 85% 25.6M 5s
228050K .......... .......... .......... .......... .......... 85% 16.7M 5s
228100K .......... .......... .......... .......... .......... 85% 36.0M 5s
228150K .......... .......... .......... .......... .......... 85% 36.5M 5s
228200K .......... .......... .......... .......... .......... 85% 23.4M 5s
228250K .......... .......... .......... .......... .......... 85% 23.1M 5s
228300K .......... .......... .......... .......... .......... 85% 27.8M 5s
228350K .......... .......... .......... .......... .......... 85% 13.9M 5s
228400K .......... .......... .......... .......... .......... 85% 29.1M 5s
228450K .......... .......... .......... .......... .......... 85% 15.6M 5s
228500K .......... .......... .......... .......... .......... 85% 16.6M 5s
228550K .......... .......... .......... .......... .......... 86% 18.3M 5s
228600K .......... .......... .......... .......... .......... 86% 13.8M 5s
228650K .......... .......... .......... .......... .......... 86% 17.1M 5s
228700K .......... .......... .......... .......... .......... 86% 15.7M 5s
228750K .......... .......... .......... .......... .......... 86% 13.3M 5s
228800K .......... .......... .......... .......... .......... 86% 17.2M 5s
228850K .......... .......... .......... .......... .......... 86% 16.0M 5s
228900K .......... .......... .......... .......... .......... 86% 18.6M 5s
228950K .......... .......... .......... .......... .......... 86% 13.1M 5s
229000K .......... .......... .......... .......... .......... 86% 10.2M 5s
229050K .......... .......... .......... .......... .......... 86% 12.9M 5s
229100K .......... .......... .......... .......... .......... 86% 7.43M 5s
229150K .......... .......... .......... .......... .......... 86% 6.51M 5s
229200K .......... .......... .......... .......... .......... 86% 6.72M 5s
229250K .......... .......... .......... .......... .......... 86% 6.85M 5s
229300K .......... .......... .......... .......... .......... 86% 7.25M 5s
229350K .......... .......... .......... .......... .......... 86% 5.04M 5s
229400K .......... .......... .......... .......... .......... 86% 9.31M 5s
229450K .......... .......... .......... .......... .......... 86% 4.23M 5s
229500K .......... .......... .......... .......... .......... 86% 10.6M 5s
229550K .......... .......... .......... .......... .......... 86% 9.87M 5s
229600K .......... .......... .......... .......... .......... 86% 9.47M 5s
229650K .......... .......... .......... .......... .......... 86% 6.58M 5s
229700K .......... .......... .......... .......... .......... 86% 5.79M 5s
229750K .......... .......... .......... .......... .......... 86% 6.24M 5s
229800K .......... .......... .......... .......... .......... 86% 7.01M 5s
229850K .......... .......... .......... .......... .......... 86% 6.99M 5s
229900K .......... .......... .......... .......... .......... 86% 9.42M 5s
229950K .......... .......... .......... .......... .......... 86% 23.2M 5s
230000K .......... .......... .......... .......... .......... 86% 38.4M 5s
230050K .......... .......... .......... .......... .......... 86% 36.8M 5s
230100K .......... .......... .......... .......... .......... 86% 24.7M 5s
230150K .......... .......... .......... .......... .......... 86% 43.5M 5s
230200K .......... .......... .......... .......... .......... 86% 22.8M 5s
230250K .......... .......... .......... .......... .......... 86% 24.9M 5s
230300K .......... .......... .......... .......... .......... 86% 24.6M 5s
230350K .......... .......... .......... .......... .......... 86% 17.2M 5s
230400K .......... .......... .......... .......... .......... 86% 17.7M 5s
230450K .......... .......... .......... .......... .......... 86% 12.3M 5s
230500K .......... .......... .......... .......... .......... 86% 18.4M 5s
230550K .......... .......... .......... .......... .......... 86% 18.9M 5s
230600K .......... .......... .......... .......... .......... 86% 16.3M 5s
230650K .......... .......... .......... .......... .......... 86% 18.3M 5s
230700K .......... .......... .......... .......... .......... 86% 17.5M 5s
230750K .......... .......... .......... .......... .......... 86% 17.5M 5s
230800K .......... .......... .......... .......... .......... 86% 18.6M 5s
230850K .......... .......... .......... .......... .......... 86% 16.5M 5s
230900K .......... .......... .......... .......... .......... 86% 15.9M 5s
230950K .......... .......... .......... .......... .......... 86% 9.21M 5s
231000K .......... .......... .......... .......... .......... 86% 11.4M 5s
231050K .......... .......... .......... .......... .......... 86% 18.3M 5s
231100K .......... .......... .......... .......... .......... 86% 17.8M 5s
231150K .......... .......... .......... .......... .......... 86% 18.4M 5s
231200K .......... .......... .......... .......... .......... 87% 17.1M 5s
231250K .......... .......... .......... .......... .......... 87% 17.7M 5s
231300K .......... .......... .......... .......... .......... 87% 17.5M 5s
231350K .......... .......... .......... .......... .......... 87% 17.3M 5s
231400K .......... .......... .......... .......... .......... 87% 16.6M 5s
231450K .......... .......... .......... .......... .......... 87% 18.8M 5s
231500K .......... .......... .......... .......... .......... 87% 17.9M 5s
231550K .......... .......... .......... .......... .......... 87% 17.9M 5s
231600K .......... .......... .......... .......... .......... 87% 16.7M 5s
231650K .......... .......... .......... .......... .......... 87% 6.63M 5s
231700K .......... .......... .......... .......... .......... 87%  107M 5s
231750K .......... .......... .......... .......... .......... 87% 18.3M 5s
231800K .......... .......... .......... .......... .......... 87% 11.6M 5s
231850K .......... .......... .......... .......... .......... 87%  110M 5s
231900K .......... .......... .......... .......... .......... 87% 18.5M 5s
231950K .......... .......... .......... .......... .......... 87% 21.6M 5s
232000K .......... .......... .......... .......... .......... 87% 24.8M 5s
232050K .......... .......... .......... .......... .......... 87% 26.4M 5s
232100K .......... .......... .......... .......... .......... 87% 22.1M 5s
232150K .......... .......... .......... .......... .......... 87% 23.2M 5s
232200K .......... .......... .......... .......... .......... 87% 18.0M 5s
232250K .......... .......... .......... .......... .......... 87% 24.8M 5s
232300K .......... .......... .......... .......... .......... 87% 23.6M 5s
232350K .......... .......... .......... .......... .......... 87% 23.4M 5s
232400K .......... .......... .......... .......... .......... 87% 30.4M 5s
232450K .......... .......... .......... .......... .......... 87% 21.1M 5s
232500K .......... .......... .......... .......... .......... 87% 23.2M 5s
232550K .......... .......... .......... .......... .......... 87% 25.8M 5s
232600K .......... .......... .......... .......... .......... 87% 23.2M 5s
232650K .......... .......... .......... .......... .......... 87% 32.9M 5s
232700K .......... .......... .......... .......... .......... 87% 16.1M 5s
232750K .......... .......... .......... .......... .......... 87% 17.7M 5s
232800K .......... .......... .......... .......... .......... 87% 25.5M 5s
232850K .......... .......... .......... .......... .......... 87% 25.1M 5s
232900K .......... .......... .......... .......... .......... 87% 72.8M 5s
232950K .......... .......... .......... .......... .......... 87% 21.8M 5s
233000K .......... .......... .......... .......... .......... 87% 38.9M 5s
233050K .......... .......... .......... .......... .......... 87% 29.6M 5s
233100K .......... .......... .......... .......... .......... 87% 23.4M 5s
233150K .......... .......... .......... .......... .......... 87% 26.4M 5s
233200K .......... .......... .......... .......... .......... 87% 33.3M 5s
233250K .......... .......... .......... .......... .......... 87% 25.8M 4s
233300K .......... .......... .......... .......... .......... 87% 29.7M 4s
233350K .......... .......... .......... .......... .......... 87% 24.1M 4s
233400K .......... .......... .......... .......... .......... 87% 36.8M 4s
233450K .......... .......... .......... .......... .......... 87% 24.5M 4s
233500K .......... .......... .......... .......... .......... 87% 25.0M 4s
233550K .......... .......... .......... .......... .......... 87% 18.3M 4s
233600K .......... .......... .......... .......... .......... 87% 16.3M 4s
233650K .......... .......... .......... .......... .......... 87% 23.0M 4s
233700K .......... .......... .......... .......... .......... 87% 16.1M 4s
233750K .......... .......... .......... .......... .......... 87% 23.9M 4s
233800K .......... .......... .......... .......... .......... 87% 18.3M 4s
233850K .......... .......... .......... .......... .......... 88% 18.4M 4s
233900K .......... .......... .......... .......... .......... 88% 22.2M 4s
233950K .......... .......... .......... .......... .......... 88% 16.8M 4s
234000K .......... .......... .......... .......... .......... 88% 24.2M 4s
234050K .......... .......... .......... .......... .......... 88% 19.2M 4s
234100K .......... .......... .......... .......... .......... 88% 21.9M 4s
234150K .......... .......... .......... .......... .......... 88% 21.1M 4s
234200K .......... .......... .......... .......... .......... 88% 20.4M 4s
234250K .......... .......... .......... .......... .......... 88% 19.4M 4s
234300K .......... .......... .......... .......... .......... 88% 28.0M 4s
234350K .......... .......... .......... .......... .......... 88% 27.9M 4s
234400K .......... .......... .......... .......... .......... 88% 50.2M 4s
234450K .......... .......... .......... .......... .......... 88% 42.5M 4s
234500K .......... .......... .......... .......... .......... 88% 79.5M 4s
234550K .......... .......... .......... .......... .......... 88% 40.4M 4s
234600K .......... .......... .......... .......... .......... 88% 31.2M 4s
234650K .......... .......... .......... .......... .......... 88% 68.3M 4s
234700K .......... .......... .......... .......... .......... 88% 13.8M 4s
234750K .......... .......... .......... .......... .......... 88% 31.7M 4s
234800K .......... .......... .......... .......... .......... 88% 73.4M 4s
234850K .......... .......... .......... .......... .......... 88% 46.5M 4s
234900K .......... .......... .......... .......... .......... 88% 66.6M 4s
234950K .......... .......... .......... .......... .......... 88% 14.3M 4s
235000K .......... .......... .......... .......... .......... 88% 66.6M 4s
235050K .......... .......... .......... .......... .......... 88% 71.3M 4s
235100K .......... .......... .......... .......... .......... 88% 26.5M 4s
235150K .......... .......... .......... .......... .......... 88% 29.7M 4s
235200K .......... .......... .......... .......... .......... 88% 38.0M 4s
235250K .......... .......... .......... .......... .......... 88% 31.1M 4s
235300K .......... .......... .......... .......... .......... 88% 18.4M 4s
235350K .......... .......... .......... .......... .......... 88% 21.1M 4s
235400K .......... .......... .......... .......... .......... 88% 53.6M 4s
235450K .......... .......... .......... .......... .......... 88% 25.9M 4s
235500K .......... .......... .......... .......... .......... 88% 26.8M 4s
235550K .......... .......... .......... .......... .......... 88% 37.0M 4s
235600K .......... .......... .......... .......... .......... 88% 26.7M 4s
235650K .......... .......... .......... .......... .......... 88% 25.7M 4s
235700K .......... .......... .......... .......... .......... 88% 31.1M 4s
235750K .......... .......... .......... .......... .......... 88% 30.1M 4s
235800K .......... .......... .......... .......... .......... 88% 23.8M 4s
235850K .......... .......... .......... .......... .......... 88% 25.9M 4s
235900K .......... .......... .......... .......... .......... 88% 34.8M 4s
235950K .......... .......... .......... .......... .......... 88% 25.2M 4s
236000K .......... .......... .......... .......... .......... 88% 30.2M 4s
236050K .......... .......... .......... .......... .......... 88% 31.7M 4s
236100K .......... .......... .......... .......... .......... 88% 17.6M 4s
236150K .......... .......... .......... .......... .......... 88% 13.6M 4s
236200K .......... .......... .......... .......... .......... 88% 16.9M 4s
236250K .......... .......... .......... .......... .......... 88% 19.9M 4s
236300K .......... .......... .......... .......... .......... 88% 22.7M 4s
236350K .......... .......... .......... .......... .......... 88% 18.5M 4s
236400K .......... .......... .......... .......... .......... 88% 32.3M 4s
236450K .......... .......... .......... .......... .......... 88% 21.2M 4s
236500K .......... .......... .......... .......... .......... 89% 41.8M 4s
236550K .......... .......... .......... .......... .......... 89% 22.6M 4s
236600K .......... .......... .......... .......... .......... 89% 18.2M 4s
236650K .......... .......... .......... .......... .......... 89% 25.5M 4s
236700K .......... .......... .......... .......... .......... 89% 17.7M 4s
236750K .......... .......... .......... .......... .......... 89% 19.6M 4s
236800K .......... .......... .......... .......... .......... 89% 26.2M 4s
236850K .......... .......... .......... .......... .......... 89% 18.7M 4s
236900K .......... .......... .......... .......... .......... 89% 25.9M 4s
236950K .......... .......... .......... .......... .......... 89% 17.5M 4s
237000K .......... .......... .......... .......... .......... 89% 21.6M 4s
237050K .......... .......... .......... .......... .......... 89% 19.8M 4s
237100K .......... .......... .......... .......... .......... 89% 10.9M 4s
237150K .......... .......... .......... .......... .......... 89% 13.1M 4s
237200K .......... .......... .......... .......... .......... 89% 15.2M 4s
237250K .......... .......... .......... .......... .......... 89% 17.7M 4s
237300K .......... .......... .......... .......... .......... 89% 13.7M 4s
237350K .......... .......... .......... .......... .......... 89% 14.1M 4s
237400K .......... .......... .......... .......... .......... 89% 18.0M 4s
237450K .......... .......... .......... .......... .......... 89% 13.2M 4s
237500K .......... .......... .......... .......... .......... 89% 17.3M 4s
237550K .......... .......... .......... .......... .......... 89% 14.3M 4s
237600K .......... .......... .......... .......... .......... 89% 17.1M 4s
237650K .......... .......... .......... .......... .......... 89% 14.1M 4s
237700K .......... .......... .......... .......... .......... 89% 14.4M 4s
237750K .......... .......... .......... .......... .......... 89% 17.5M 4s
237800K .......... .......... .......... .......... .......... 89% 10.9M 4s
237850K .......... .......... .......... .......... .......... 89% 22.2M 4s
237900K .......... .......... .......... .......... .......... 89% 13.1M 4s
237950K .......... .......... .......... .......... .......... 89% 38.3M 4s
238000K .......... .......... .......... .......... .......... 89% 22.6M 4s
238050K .......... .......... .......... .......... .......... 89% 32.2M 4s
238100K .......... .......... .......... .......... .......... 89% 31.1M 4s
238150K .......... .......... .......... .......... .......... 89% 28.8M 4s
238200K .......... .......... .......... .......... .......... 89% 23.7M 4s
238250K .......... .......... .......... .......... .......... 89% 38.9M 4s
238300K .......... .......... .......... .......... .......... 89% 25.2M 4s
238350K .......... .......... .......... .......... .......... 89% 26.6M 4s
238400K .......... .......... .......... .......... .......... 89% 25.5M 4s
238450K .......... .......... .......... .......... .......... 89% 25.1M 4s
238500K .......... .......... .......... .......... .......... 89% 40.1M 4s
238550K .......... .......... .......... .......... .......... 89% 26.4M 4s
238600K .......... .......... .......... .......... .......... 89% 24.1M 4s
238650K .......... .......... .......... .......... .......... 89% 38.5M 4s
238700K .......... .......... .......... .......... .......... 89% 22.9M 4s
238750K .......... .......... .......... .......... .......... 89% 26.2M 4s
238800K .......... .......... .......... .......... .......... 89% 24.8M 4s
238850K .......... .......... .......... .......... .......... 89% 24.1M 4s
238900K .......... .......... .......... .......... .......... 89% 29.6M 4s
238950K .......... .......... .......... .......... .......... 89% 23.2M 4s
239000K .......... .......... .......... .......... .......... 89% 36.1M 4s
239050K .......... .......... .......... .......... .......... 89% 76.6M 4s
239100K .......... .......... .......... .......... .......... 89% 14.8M 4s
239150K .......... .......... .......... .......... .......... 89%  118M 4s
239200K .......... .......... .......... .......... .......... 90% 25.0M 4s
239250K .......... .......... .......... .......... .......... 90% 26.6M 4s
239300K .......... .......... .......... .......... .......... 90%  105M 4s
239350K .......... .......... .......... .......... .......... 90% 21.8M 4s
239400K .......... .......... .......... .......... .......... 90% 44.5M 4s
239450K .......... .......... .......... .......... .......... 90% 23.1M 4s
239500K .......... .......... .......... .......... .......... 90% 26.9M 4s
239550K .......... .......... .......... .......... .......... 90% 29.0M 4s
239600K .......... .......... .......... .......... .......... 90% 25.3M 4s
239650K .......... .......... .......... .......... .......... 90% 43.3M 4s
239700K .......... .......... .......... .......... .......... 90% 34.9M 4s
239750K .......... .......... .......... .......... .......... 90% 36.1M 4s
239800K .......... .......... .......... .......... .......... 90% 36.8M 4s
239850K .......... .......... .......... .......... .......... 90% 33.9M 4s
239900K .......... .......... .......... .......... .......... 90% 51.1M 4s
239950K .......... .......... .......... .......... .......... 90% 36.6M 3s
240000K .......... .......... .......... .......... .......... 90% 29.3M 3s
240050K .......... .......... .......... .......... .......... 90% 51.5M 3s
240100K .......... .......... .......... .......... .......... 90% 33.7M 3s
240150K .......... .......... .......... .......... .......... 90% 40.1M 3s
240200K .......... .......... .......... .......... .......... 90% 31.9M 3s
240250K .......... .......... .......... .......... .......... 90% 38.9M 3s
240300K .......... .......... .......... .......... .......... 90% 50.2M 3s
240350K .......... .......... .......... .......... .......... 90% 33.8M 3s
240400K .......... .......... .......... .......... .......... 90% 38.2M 3s
240450K .......... .......... .......... .......... .......... 90% 34.5M 3s
240500K .......... .......... .......... .......... .......... 90% 35.9M 3s
240550K .......... .......... .......... .......... .......... 90% 22.6M 3s
240600K .......... .......... .......... .......... .......... 90% 15.6M 3s
240650K .......... .......... .......... .......... .......... 90% 11.0M 3s
240700K .......... .......... .......... .......... .......... 90% 14.4M 3s
240750K .......... .......... .......... .......... .......... 90% 20.0M 3s
240800K .......... .......... .......... .......... .......... 90% 24.4M 3s
240850K .......... .......... .......... .......... .......... 90% 16.8M 3s
240900K .......... .......... .......... .......... .......... 90% 25.1M 3s
240950K .......... .......... .......... .......... .......... 90% 18.8M 3s
241000K .......... .......... .......... .......... .......... 90% 24.4M 3s
241050K .......... .......... .......... .......... .......... 90% 25.8M 3s
241100K .......... .......... .......... .......... .......... 90% 20.2M 3s
241150K .......... .......... .......... .......... .......... 90% 21.8M 3s
241200K .......... .......... .......... .......... .......... 90% 21.2M 3s
241250K .......... .......... .......... .......... .......... 90% 27.3M 3s
241300K .......... .......... .......... .......... .......... 90% 19.3M 3s
241350K .......... .......... .......... .......... .......... 90% 24.0M 3s
241400K .......... .......... .......... .......... .......... 90% 25.2M 3s
241450K .......... .......... .......... .......... .......... 90% 16.4M 3s
241500K .......... .......... .......... .......... .......... 90% 67.9M 3s
241550K .......... .......... .......... .......... .......... 90% 71.1M 3s
241600K .......... .......... .......... .......... .......... 90% 35.1M 3s
241650K .......... .......... .......... .......... .......... 90% 25.8M 3s
241700K .......... .......... .......... .......... .......... 90% 20.9M 3s
241750K .......... .......... .......... .......... .......... 90% 10.1M 3s
241800K .......... .......... .......... .......... .......... 90% 15.3M 3s
241850K .......... .......... .......... .......... .......... 91% 10.9M 3s
241900K .......... .......... .......... .......... .......... 91% 15.7M 3s
241950K .......... .......... .......... .......... .......... 91% 12.0M 3s
242000K .......... .......... .......... .......... .......... 91% 16.4M 3s
242050K .......... .......... .......... .......... .......... 91% 13.0M 3s
242100K .......... .......... .......... .......... .......... 91% 15.5M 3s
242150K .......... .......... .......... .......... .......... 91% 23.3M 3s
242200K .......... .......... .......... .......... .......... 91% 17.9M 3s
242250K .......... .......... .......... .......... .......... 91% 22.5M 3s
242300K .......... .......... .......... .......... .......... 91% 14.2M 3s
242350K .......... .......... .......... .......... .......... 91% 12.6M 3s
242400K .......... .......... .......... .......... .......... 91% 22.9M 3s
242450K .......... .......... .......... .......... .......... 91% 18.5M 3s
242500K .......... .......... .......... .......... .......... 91% 23.3M 3s
242550K .......... .......... .......... .......... .......... 91% 20.6M 3s
242600K .......... .......... .......... .......... .......... 91% 12.0M 3s
242650K .......... .......... .......... .......... .......... 91% 23.7M 3s
242700K .......... .......... .......... .......... .......... 91% 21.0M 3s
242750K .......... .......... .......... .......... .......... 91% 20.6M 3s
242800K .......... .......... .......... .......... .......... 91% 12.4M 3s
242850K .......... .......... .......... .......... .......... 91% 23.2M 3s
242900K .......... .......... .......... .......... .......... 91% 23.1M 3s
242950K .......... .......... .......... .......... .......... 91% 22.5M 3s
243000K .......... .......... .......... .......... .......... 91% 18.1M 3s
243050K .......... .......... .......... .......... .......... 91% 21.0M 3s
243100K .......... .......... .......... .......... .......... 91% 15.2M 3s
243150K .......... .......... .......... .......... .......... 91% 8.44M 3s
243200K .......... .......... .......... .......... .......... 91%  120M 3s
243250K .......... .......... .......... .......... .......... 91% 8.79M 3s
243300K .......... .......... .......... .......... .......... 91%  151M 3s
243350K .......... .......... .......... .......... .......... 91% 15.4M 3s
243400K .......... .......... .......... .......... .......... 91% 13.5M 3s
243450K .......... .......... .......... .......... .......... 91% 60.3M 3s
243500K .......... .......... .......... .......... .......... 91% 29.5M 3s
243550K .......... .......... .......... .......... .......... 91% 24.1M 3s
243600K .......... .......... .......... .......... .......... 91% 18.9M 3s
243650K .......... .......... .......... .......... .......... 91% 29.9M 3s
243700K .......... .......... .......... .......... .......... 91% 23.8M 3s
243750K .......... .......... .......... .......... .......... 91% 39.4M 3s
243800K .......... .......... .......... .......... .......... 91% 29.9M 3s
243850K .......... .......... .......... .......... .......... 91% 27.4M 3s
243900K .......... .......... .......... .......... .......... 91% 28.6M 3s
243950K .......... .......... .......... .......... .......... 91% 29.2M 3s
244000K .......... .......... .......... .......... .......... 91% 29.0M 3s
244050K .......... .......... .......... .......... .......... 91% 27.8M 3s
244100K .......... .......... .......... .......... .......... 91% 30.1M 3s
244150K .......... .......... .......... .......... .......... 91% 32.1M 3s
244200K .......... .......... .......... .......... .......... 91% 26.3M 3s
244250K .......... .......... .......... .......... .......... 91% 45.9M 3s
244300K .......... .......... .......... .......... .......... 91% 27.8M 3s
244350K .......... .......... .......... .......... .......... 91% 30.0M 3s
244400K .......... .......... .......... .......... .......... 91% 21.5M 3s
244450K .......... .......... .......... .......... .......... 91% 17.9M 3s
244500K .......... .......... .......... .......... .......... 92% 29.9M 3s
244550K .......... .......... .......... .......... .......... 92% 27.7M 3s
244600K .......... .......... .......... .......... .......... 92% 59.8M 3s
244650K .......... .......... .......... .......... .......... 92% 30.4M 3s
244700K .......... .......... .......... .......... .......... 92% 23.9M 3s
244750K .......... .......... .......... .......... .......... 92% 27.3M 3s
244800K .......... .......... .......... .......... .......... 92%  114M 3s
244850K .......... .......... .......... .......... .......... 92% 22.5M 3s
244900K .......... .......... .......... .......... .......... 92% 28.3M 3s
244950K .......... .......... .......... .......... .......... 92% 23.4M 3s
245000K .......... .......... .......... .......... .......... 92%  115M 3s
245050K .......... .......... .......... .......... .......... 92% 27.3M 3s
245100K .......... .......... .......... .......... .......... 92% 23.5M 3s
245150K .......... .......... .......... .......... .......... 92% 87.1M 3s
245200K .......... .......... .......... .......... .......... 92% 25.7M 3s
245250K .......... .......... .......... .......... .......... 92% 25.3M 3s
245300K .......... .......... .......... .......... .......... 92% 73.0M 3s
245350K .......... .......... .......... .......... .......... 92% 22.1M 3s
245400K .......... .......... .......... .......... .......... 92% 31.5M 3s
245450K .......... .......... .......... .......... .......... 92% 42.5M 3s
245500K .......... .......... .......... .......... .......... 92% 26.7M 3s
245550K .......... .......... .......... .......... .......... 92% 24.4M 3s
245600K .......... .......... .......... .......... .......... 92% 65.0M 3s
245650K .......... .......... .......... .......... .......... 92% 24.1M 3s
245700K .......... .......... .......... .......... .......... 92% 20.6M 3s
245750K .......... .......... .......... .......... .......... 92%  105M 3s
245800K .......... .......... .......... .......... .......... 92% 26.5M 3s
245850K .......... .......... .......... .......... .......... 92% 23.9M 3s
245900K .......... .......... .......... .......... .......... 92% 45.9M 3s
245950K .......... .......... .......... .......... .......... 92% 21.2M 3s
246000K .......... .......... .......... .......... .......... 92% 47.2M 3s
246050K .......... .......... .......... .......... .......... 92% 26.0M 3s
246100K .......... .......... .......... .......... .......... 92% 26.3M 3s
246150K .......... .......... .......... .......... .......... 92% 52.1M 3s
246200K .......... .......... .......... .......... .......... 92% 16.2M 3s
246250K .......... .......... .......... .......... .......... 92% 37.1M 3s
246300K .......... .......... .......... .......... .......... 92% 22.7M 3s
246350K .......... .......... .......... .......... .......... 92% 35.1M 3s
246400K .......... .......... .......... .......... .......... 92% 24.1M 3s
246450K .......... .......... .......... .......... .......... 92% 24.5M 3s
246500K .......... .......... .......... .......... .......... 92% 22.3M 3s
246550K .......... .......... .......... .......... .......... 92% 48.8M 3s
246600K .......... .......... .......... .......... .......... 92% 19.6M 3s
246650K .......... .......... .......... .......... .......... 92% 20.7M 3s
246700K .......... .......... .......... .......... .......... 92% 96.9M 3s
246750K .......... .......... .......... .......... .......... 92% 17.2M 3s
246800K .......... .......... .......... .......... .......... 92% 19.7M 3s
246850K .......... .......... .......... .......... .......... 92% 29.8M 3s
246900K .......... .......... .......... .......... .......... 92% 36.1M 3s
246950K .......... .......... .......... .......... .......... 92% 20.4M 2s
247000K .......... .......... .......... .......... .......... 92% 20.5M 2s
247050K .......... .......... .......... .......... .......... 92% 67.0M 2s
247100K .......... .......... .......... .......... .......... 92% 20.2M 2s
247150K .......... .......... .......... .......... .......... 93% 22.6M 2s
247200K .......... .......... .......... .......... .......... 93% 64.4M 2s
247250K .......... .......... .......... .......... .......... 93% 21.3M 2s
247300K .......... .......... .......... .......... .......... 93% 21.2M 2s
247350K .......... .......... .......... .......... .......... 93% 75.4M 2s
247400K .......... .......... .......... .......... .......... 93% 20.9M 2s
247450K .......... .......... .......... .......... .......... 93% 19.4M 2s
247500K .......... .......... .......... .......... .......... 93% 80.3M 2s
247550K .......... .......... .......... .......... .......... 93% 19.2M 2s
247600K .......... .......... .......... .......... .......... 93% 70.8M 2s
247650K .......... .......... .......... .......... .......... 93% 18.4M 2s
247700K .......... .......... .......... .......... .......... 93% 19.3M 2s
247750K .......... .......... .......... .......... .......... 93% 82.0M 2s
247800K .......... .......... .......... .......... .......... 93% 19.0M 2s
247850K .......... .......... .......... .......... .......... 93% 57.3M 2s
247900K .......... .......... .......... .......... .......... 93% 20.4M 2s
247950K .......... .......... .......... .......... .......... 93% 20.2M 2s
248000K .......... .......... .......... .......... .......... 93% 65.1M 2s
248050K .......... .......... .......... .......... .......... 93% 20.5M 2s
248100K .......... .......... .......... .......... .......... 93% 23.0M 2s
248150K .......... .......... .......... .......... .......... 93% 41.6M 2s
248200K .......... .......... .......... .......... .......... 93% 20.0M 2s
248250K .......... .......... .......... .......... .......... 93% 27.6M 2s
248300K .......... .......... .......... .......... .......... 93% 38.9M 2s
248350K .......... .......... .......... .......... .......... 93% 18.7M 2s
248400K .......... .......... .......... .......... .......... 93% 90.0M 2s
248450K .......... .......... .......... .......... .......... 93% 19.8M 2s
248500K .......... .......... .......... .......... .......... 93% 25.4M 2s
248550K .......... .......... .......... .......... .......... 93% 41.2M 2s
248600K .......... .......... .......... .......... .......... 93% 18.4M 2s
248650K .......... .......... .......... .......... .......... 93% 91.6M 2s
248700K .......... .......... .......... .......... .......... 93% 19.5M 2s
248750K .......... .......... .......... .......... .......... 93% 90.8M 2s
248800K .......... .......... .......... .......... .......... 93% 16.7M 2s
248850K .......... .......... .......... .......... .......... 93% 18.2M 2s
248900K .......... .......... .......... .......... .......... 93% 49.5M 2s
248950K .......... .......... .......... .......... .......... 93% 10.6M 2s
249000K .......... .......... .......... .......... .......... 93% 77.6M 2s
249050K .......... .......... .......... .......... .......... 93% 75.6M 2s
249100K .......... .......... .......... .......... .......... 93% 24.6M 2s
249150K .......... .......... .......... .......... .......... 93% 23.8M 2s
249200K .......... .......... .......... .......... .......... 93% 36.5M 2s
249250K .......... .......... .......... .......... .......... 93% 21.6M 2s
249300K .......... .......... .......... .......... .......... 93% 24.6M 2s
249350K .......... .......... .......... .......... .......... 93% 19.1M 2s
249400K .......... .......... .......... .......... .......... 93% 60.2M 2s
249450K .......... .......... .......... .......... .......... 93% 18.0M 2s
249500K .......... .......... .......... .......... .......... 93% 23.2M 2s
249550K .......... .......... .......... .......... .......... 93% 16.1M 2s
249600K .......... .......... .......... .......... .......... 93% 18.5M 2s
249650K .......... .......... .......... .......... .......... 93% 21.8M 2s
249700K .......... .......... .......... .......... .......... 93% 18.2M 2s
249750K .......... .......... .......... .......... .......... 93% 48.5M 2s
249800K .......... .......... .......... .......... .......... 94% 20.4M 2s
249850K .......... .......... .......... .......... .......... 94% 16.4M 2s
249900K .......... .......... .......... .......... .......... 94% 20.4M 2s
249950K .......... .......... .......... .......... .......... 94% 8.79M 2s
250000K .......... .......... .......... .......... .......... 94%  139M 2s
250050K .......... .......... .......... .......... .......... 94%  143M 2s
250100K .......... .......... .......... .......... .......... 94% 15.3M 2s
250150K .......... .......... .......... .......... .......... 94% 67.4M 2s
250200K .......... .......... .......... .......... .......... 94% 21.7M 2s
250250K .......... .......... .......... .......... .......... 94% 87.4M 2s
250300K .......... .......... .......... .......... .......... 94% 34.5M 2s
250350K .......... .......... .......... .......... .......... 94% 32.5M 2s
250400K .......... .......... .......... .......... .......... 94% 35.7M 2s
250450K .......... .......... .......... .......... .......... 94% 18.3M 2s
250500K .......... .......... .......... .......... .......... 94%  149M 2s
250550K .......... .......... .......... .......... .......... 94% 44.5M 2s
250600K .......... .......... .......... .......... .......... 94% 39.2M 2s
250650K .......... .......... .......... .......... .......... 94% 30.8M 2s
250700K .......... .......... .......... .......... .......... 94% 35.6M 2s
250750K .......... .......... .......... .......... .......... 94% 36.5M 2s
250800K .......... .......... .......... .......... .......... 94% 44.1M 2s
250850K .......... .......... .......... .......... .......... 94% 28.1M 2s
250900K .......... .......... .......... .......... .......... 94% 41.5M 2s
250950K .......... .......... .......... .......... .......... 94% 25.0M 2s
251000K .......... .......... .......... .......... .......... 94% 39.6M 2s
251050K .......... .......... .......... .......... .......... 94% 41.7M 2s
251100K .......... .......... .......... .......... .......... 94% 26.6M 2s
251150K .......... .......... .......... .......... .......... 94% 48.6M 2s
251200K .......... .......... .......... .......... .......... 94% 39.0M 2s
251250K .......... .......... .......... .......... .......... 94% 42.3M 2s
251300K .......... .......... .......... .......... .......... 94% 26.6M 2s
251350K .......... .......... .......... .......... .......... 94% 40.9M 2s
251400K .......... .......... .......... .......... .......... 94% 44.8M 2s
251450K .......... .......... .......... .......... .......... 94% 25.8M 2s
251500K .......... .......... .......... .......... .......... 94% 47.1M 2s
251550K .......... .......... .......... .......... .......... 94% 44.5M 2s
251600K .......... .......... .......... .......... .......... 94% 25.9M 2s
251650K .......... .......... .......... .......... .......... 94% 53.5M 2s
251700K .......... .......... .......... .......... .......... 94% 27.6M 2s
251750K .......... .......... .......... .......... .......... 94% 41.8M 2s
251800K .......... .......... .......... .......... .......... 94% 37.3M 2s
251850K .......... .......... .......... .......... .......... 94% 32.9M 2s
251900K .......... .......... .......... .......... .......... 94% 71.1M 2s
251950K .......... .......... .......... .......... .......... 94% 24.6M 2s
252000K .......... .......... .......... .......... .......... 94% 79.0M 2s
252050K .......... .......... .......... .......... .......... 94% 26.8M 2s
252100K .......... .......... .......... .......... .......... 94% 65.7M 2s
252150K .......... .......... .......... .......... .......... 94% 27.9M 2s
252200K .......... .......... .......... .......... .......... 94% 26.0M 2s
252250K .......... .......... .......... .......... .......... 94% 63.4M 2s
252300K .......... .......... .......... .......... .......... 94% 28.8M 2s
252350K .......... .......... .......... .......... .......... 94% 63.5M 2s
252400K .......... .......... .......... .......... .......... 94% 29.2M 2s
252450K .......... .......... .......... .......... .......... 95% 64.2M 2s
252500K .......... .......... .......... .......... .......... 95% 11.7M 2s
252550K .......... .......... .......... .......... .......... 95%  114M 2s
252600K .......... .......... .......... .......... .......... 95%  120M 2s
252650K .......... .......... .......... .......... .......... 95%  105M 2s
252700K .......... .......... .......... .......... .......... 95% 30.1M 2s
252750K .......... .......... .......... .......... .......... 95% 21.1M 2s
252800K .......... .......... .......... .......... .......... 95% 24.7M 2s
252850K .......... .......... .......... .......... .......... 95% 26.2M 2s
252900K .......... .......... .......... .......... .......... 95% 30.2M 2s
252950K .......... .......... .......... .......... .......... 95% 23.7M 2s
253000K .......... .......... .......... .......... .......... 95% 62.5M 2s
253050K .......... .......... .......... .......... .......... 95% 28.9M 2s
253100K .......... .......... .......... .......... .......... 95% 24.4M 2s
253150K .......... .......... .......... .......... .......... 95% 28.5M 2s
253200K .......... .......... .......... .......... .......... 95% 26.6M 2s
253250K .......... .......... .......... .......... .......... 95% 37.2M 2s
253300K .......... .......... .......... .......... .......... 95% 38.3M 2s
253350K .......... .......... .......... .......... .......... 95% 33.5M 2s
253400K .......... .......... .......... .......... .......... 95% 36.9M 2s
253450K .......... .......... .......... .......... .......... 95% 30.7M 2s
253500K .......... .......... .......... .......... .......... 95% 30.3M 2s
253550K .......... .......... .......... .......... .......... 95% 32.9M 2s
253600K .......... .......... .......... .......... .......... 95% 38.3M 2s
253650K .......... .......... .......... .......... .......... 95% 33.6M 2s
253700K .......... .......... .......... .......... .......... 95% 30.9M 2s
253750K .......... .......... .......... .......... .......... 95% 33.1M 2s
253800K .......... .......... .......... .......... .......... 95% 35.7M 2s
253850K .......... .......... .......... .......... .......... 95% 27.1M 2s
253900K .......... .......... .......... .......... .......... 95% 38.3M 2s
253950K .......... .......... .......... .......... .......... 95% 23.9M 2s
254000K .......... .......... .......... .......... .......... 95% 27.7M 2s
254050K .......... .......... .......... .......... .......... 95% 29.5M 2s
254100K .......... .......... .......... .......... .......... 95% 36.6M 2s
254150K .......... .......... .......... .......... .......... 95% 61.7M 2s
254200K .......... .......... .......... .......... .......... 95% 39.3M 2s
254250K .......... .......... .......... .......... .......... 95%  119M 1s
254300K .......... .......... .......... .......... .......... 95% 36.5M 1s
254350K .......... .......... .......... .......... .......... 95% 97.4M 1s
254400K .......... .......... .......... .......... .......... 95% 34.2M 1s
254450K .......... .......... .......... .......... .......... 95% 16.1M 1s
254500K .......... .......... .......... .......... .......... 95%  132M 1s
254550K .......... .......... .......... .......... .......... 95%  118M 1s
254600K .......... .......... .......... .......... .......... 95% 21.8M 1s
254650K .......... .......... .......... .......... .......... 95%  114M 1s
254700K .......... .......... .......... .......... .......... 95% 40.0M 1s
254750K .......... .......... .......... .......... .......... 95%  121M 1s
254800K .......... .......... .......... .......... .......... 95% 33.6M 1s
254850K .......... .......... .......... .......... .......... 95% 38.1M 1s
254900K .......... .......... .......... .......... .......... 95% 42.7M 1s
254950K .......... .......... .......... .......... .......... 95% 25.6M 1s
255000K .......... .......... .......... .......... .......... 95% 39.0M 1s
255050K .......... .......... .......... .......... .......... 95% 42.1M 1s
255100K .......... .......... .......... .......... .......... 96% 37.4M 1s
255150K .......... .......... .......... .......... .......... 96% 25.5M 1s
255200K .......... .......... .......... .......... .......... 96% 39.4M 1s
255250K .......... .......... .......... .......... .......... 96% 39.6M 1s
255300K .......... .......... .......... .......... .......... 96% 40.1M 1s
255350K .......... .......... .......... .......... .......... 96% 33.3M 1s
255400K .......... .......... .......... .......... .......... 96% 30.4M 1s
255450K .......... .......... .......... .......... .......... 96% 35.4M 1s
255500K .......... .......... .......... .......... .......... 96% 40.9M 1s
255550K .......... .......... .......... .......... .......... 96% 33.2M 1s
255600K .......... .......... .......... .......... .......... 96% 29.8M 1s
255650K .......... .......... .......... .......... .......... 96% 39.0M 1s
255700K .......... .......... .......... .......... .......... 96% 35.0M 1s
255750K .......... .......... .......... .......... .......... 96% 27.8M 1s
255800K .......... .......... .......... .......... .......... 96% 27.9M 1s
255850K .......... .......... .......... .......... .......... 96% 40.1M 1s
255900K .......... .......... .......... .......... .......... 96% 32.4M 1s
255950K .......... .......... .......... .......... .......... 96% 42.6M 1s
256000K .......... .......... .......... .......... .......... 96% 34.5M 1s
256050K .......... .......... .......... .......... .......... 96% 33.5M 1s
256100K .......... .......... .......... .......... .......... 96% 23.4M 1s
256150K .......... .......... .......... .......... .......... 96% 30.2M 1s
256200K .......... .......... .......... .......... .......... 96% 19.1M 1s
256250K .......... .......... .......... .......... .......... 96% 22.3M 1s
256300K .......... .......... .......... .......... .......... 96% 26.3M 1s
256350K .......... .......... .......... .......... .......... 96% 20.7M 1s
256400K .......... .......... .......... .......... .......... 96% 22.5M 1s
256450K .......... .......... .......... .......... .......... 96% 20.4M 1s
256500K .......... .......... .......... .......... .......... 96% 20.3M 1s
256550K .......... .......... .......... .......... .......... 96% 32.3M 1s
256600K .......... .......... .......... .......... .......... 96% 19.9M 1s
256650K .......... .......... .......... .......... .......... 96% 20.8M 1s
256700K .......... .......... .......... .......... .......... 96% 30.9M 1s
256750K .......... .......... .......... .......... .......... 96% 29.7M 1s
256800K .......... .......... .......... .......... .......... 96% 28.2M 1s
256850K .......... .......... .......... .......... .......... 96% 20.6M 1s
256900K .......... .......... .......... .......... .......... 96% 25.5M 1s
256950K .......... .......... .......... .......... .......... 96% 55.7M 1s
257000K .......... .......... .......... .......... .......... 96% 21.0M 1s
257050K .......... .......... .......... .......... .......... 96% 21.0M 1s
257100K .......... .......... .......... .......... .......... 96% 47.0M 1s
257150K .......... .......... .......... .......... .......... 96% 25.6M 1s
257200K .......... .......... .......... .......... .......... 96% 19.4M 1s
257250K .......... .......... .......... .......... .......... 96% 52.0M 1s
257300K .......... .......... .......... .......... .......... 96% 20.7M 1s
257350K .......... .......... .......... .......... .......... 96% 22.5M 1s
257400K .......... .......... .......... .......... .......... 96% 64.2M 1s
257450K .......... .......... .......... .......... .......... 96% 18.4M 1s
257500K .......... .......... .......... .......... .......... 96% 19.6M 1s
257550K .......... .......... .......... .......... .......... 96% 14.7M 1s
257600K .......... .......... .......... .......... .......... 96% 26.3M 1s
257650K .......... .......... .......... .......... .......... 96% 22.3M 1s
257700K .......... .......... .......... .......... .......... 96%  120M 1s
257750K .......... .......... .......... .......... .......... 96% 11.7M 1s
257800K .......... .......... .......... .......... .......... 97% 28.9M 1s
257850K .......... .......... .......... .......... .......... 97% 13.9M 1s
257900K .......... .......... .......... .......... .......... 97% 20.1M 1s
257950K .......... .......... .......... .......... .......... 97% 17.7M 1s
258000K .......... .......... .......... .......... .......... 97% 21.5M 1s
258050K .......... .......... .......... .......... .......... 97% 19.1M 1s
258100K .......... .......... .......... .......... .......... 97% 18.7M 1s
258150K .......... .......... .......... .......... .......... 97% 17.6M 1s
258200K .......... .......... .......... .......... .......... 97% 22.6M 1s
258250K .......... .......... .......... .......... .......... 97% 18.7M 1s
258300K .......... .......... .......... .......... .......... 97% 16.3M 1s
258350K .......... .......... .......... .......... .......... 97% 20.3M 1s
258400K .......... .......... .......... .......... .......... 97% 14.7M 1s
258450K .......... .......... .......... .......... .......... 97% 6.29M 1s
258500K .......... .......... .......... .......... .......... 97% 10.6M 1s
258550K .......... .......... .......... .......... .......... 97% 10.6M 1s
258600K .......... .......... .......... .......... .......... 97% 10.1M 1s
258650K .......... .......... .......... .......... .......... 97% 10.3M 1s
258700K .......... .......... .......... .......... .......... 97% 7.90M 1s
258750K .......... .......... .......... .......... .......... 97% 10.9M 1s
258800K .......... .......... .......... .......... .......... 97% 11.5M 1s
258850K .......... .......... .......... .......... .......... 97% 31.9M 1s
258900K .......... .......... .......... .......... .......... 97% 19.7M 1s
258950K .......... .......... .......... .......... .......... 97% 12.3M 1s
259000K .......... .......... .......... .......... .......... 97% 16.1M 1s
259050K .......... .......... .......... .......... .......... 97% 10.4M 1s
259100K .......... .......... .......... .......... .......... 97% 13.8M 1s
259150K .......... .......... .......... .......... .......... 97% 18.3M 1s
259200K .......... .......... .......... .......... .......... 97% 15.0M 1s
259250K .......... .......... .......... .......... .......... 97% 18.1M 1s
259300K .......... .......... .......... .......... .......... 97% 20.1M 1s
259350K .......... .......... .......... .......... .......... 97% 14.4M 1s
259400K .......... .......... .......... .......... .......... 97% 17.6M 1s
259450K .......... .......... .......... .......... .......... 97% 18.8M 1s
259500K .......... .......... .......... .......... .......... 97% 19.2M 1s
259550K .......... .......... .......... .......... .......... 97% 19.5M 1s
259600K .......... .......... .......... .......... .......... 97% 13.6M 1s
259650K .......... .......... .......... .......... .......... 97% 19.2M 1s
259700K .......... .......... .......... .......... .......... 97% 24.9M 1s
259750K .......... .......... .......... .......... .......... 97% 47.5M 1s
259800K .......... .......... .......... .......... .......... 97% 84.4M 1s
259850K .......... .......... .......... .......... .......... 97% 50.6M 1s
259900K .......... .......... .......... .......... .......... 97% 55.0M 1s
259950K .......... .......... .......... .......... .......... 97% 86.4M 1s
260000K .......... .......... .......... .......... .......... 97% 26.2M 1s
260050K .......... .......... .......... .......... .......... 97% 14.0M 1s
260100K .......... .......... .......... .......... .......... 97% 40.6M 1s
260150K .......... .......... .......... .......... .......... 97% 23.3M 1s
260200K .......... .......... .......... .......... .......... 97% 26.5M 1s
260250K .......... .......... .......... .......... .......... 97% 18.5M 1s
260300K .......... .......... .......... .......... .......... 97% 40.4M 1s
260350K .......... .......... .......... .......... .......... 97% 20.2M 1s
260400K .......... .......... .......... .......... .......... 97% 15.7M 1s
260450K .......... .......... .......... .......... .......... 98% 20.8M 1s
260500K .......... .......... .......... .......... .......... 98% 15.6M 1s
260550K .......... .......... .......... .......... .......... 98% 18.1M 1s
260600K .......... .......... .......... .......... .......... 98% 19.1M 1s
260650K .......... .......... .......... .......... .......... 98% 18.3M 1s
260700K .......... .......... .......... .......... .......... 98% 15.5M 1s
260750K .......... .......... .......... .......... .......... 98% 18.1M 1s
260800K .......... .......... .......... .......... .......... 98% 19.9M 1s
260850K .......... .......... .......... .......... .......... 98% 14.4M 1s
260900K .......... .......... .......... .......... .......... 98% 18.8M 1s
260950K .......... .......... .......... .......... .......... 98% 20.9M 1s
261000K .......... .......... .......... .......... .......... 98% 14.6M 1s
261050K .......... .......... .......... .......... .......... 98% 8.38M 1s
261100K .......... .......... .......... .......... .......... 98% 9.55M 1s
261150K .......... .......... .......... .......... .......... 98% 12.9M 1s
261200K .......... .......... .......... .......... .......... 98% 10.9M 1s
261250K .......... .......... .......... .......... .......... 98% 12.9M 1s
261300K .......... .......... .......... .......... .......... 98% 12.4M 1s
261350K .......... .......... .......... .......... .......... 98% 9.49M 1s
261400K .......... .......... .......... .......... .......... 98% 12.1M 1s
261450K .......... .......... .......... .......... .......... 98% 10.9M 1s
261500K .......... .......... .......... .......... .......... 98% 12.6M 1s
261550K .......... .......... .......... .......... .......... 98% 10.1M 1s
261600K .......... .......... .......... .......... .......... 98% 27.9M 1s
261650K .......... .......... .......... .......... .......... 98% 11.0M 1s
261700K .......... .......... .......... .......... .......... 98% 24.6M 1s
261750K .......... .......... .......... .......... .......... 98% 17.5M 1s
261800K .......... .......... .......... .......... .......... 98% 17.1M 1s
261850K .......... .......... .......... .......... .......... 98% 15.4M 0s
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261950K .......... .......... .......... .......... .......... 98% 17.3M 0s
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262150K .......... .......... .......... .......... .......... 98% 18.8M 0s
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262250K .......... .......... .......... .......... .......... 98% 16.7M 0s
262300K .......... .......... .......... .......... .......... 98% 26.1M 0s
262350K .......... .......... .......... .......... .......... 98% 17.4M 0s
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262450K .......... .......... .......... .......... .......... 98% 17.4M 0s
262500K .......... .......... .......... .......... .......... 98% 15.2M 0s
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262700K .......... .......... .......... .......... .......... 98% 27.0M 0s
262750K .......... .......... .......... .......... .......... 98% 34.9M 0s
262800K .......... .......... .......... .......... .......... 98% 40.3M 0s
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264750K .......... .......... .......... .......... .......... 99% 29.5M 0s
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264850K .......... .......... .......... .......... .......... 99% 29.9M 0s
264900K .......... .......... .......... .......... .......... 99% 40.9M 0s
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265000K .......... .......... .......... .......... .......... 99% 32.5M 0s
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265250K .......... .......... .......... .......... .......... 99% 24.7M 0s
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265700K .......... .......... .......... .......... .......... 99% 44.4M 0s
265750K .......... .......... ..........                      100% 34.5M=34s

2024-06-18 21:17:25 (7.72 MB/s) - ‘ESPbeta.tgz’ saved [272159479/272159479]

+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/config/
+ ./makeEnv

ESP runtime AutoConfigurator

CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0  with contents:
bin
include
lib
share


Info: Python exec /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python found!
Info: Python header /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11/Python.h found!
Info: Python library /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib/libpython3.11.so found!

ESP_ARCH = LINUX64
ESP_ROOT = /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad
EFCOMP   = ifort

CARCH    = LINUX64
CASROOT  = /home/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH  = .
CASREV   = 7.8

PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11

+ source /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad
++ ESP_ROOT=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/test:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/lib/perl/bin:/home/jenkins/util/tsfoil:/home/jenkins/util/refine/build_parallel/install/bin:/home/jenkins/util/pointwise/Pointwise2023.2:/home/jenkins/util/mystran/MYSTRAN/Binaries:/home/jenkins/util/julia/julia/bin:/home/jenkins/util/delaundo/delaundo/src:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin:/home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/X86_64_ICC/:/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/bin:/opt/intel/oneapi/mpi/2021.11/bin:/opt/intel/oneapi/mkl/2024.0/bin/:/opt/intel/oneapi/dev-utilities/2024.0/bin:/opt/intel/oneapi/debugger/2024.0/opt/debugger/bin:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/bin:/opt/intel/oneapi/compiler/2024.0/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/snap/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ PYTHONINC=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
++ export 'PYTHONLIB=-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ PYTHONLIB='-L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11'
++ export PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/pyESP:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/pyCAPS:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/pyESP:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/CAPS/pyCAPS:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/OpenCSM/trunk/pyOCSM:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=ifort
++ EFCOMP=ifort
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib:/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:/opt/intel/oneapi/tbb/2021.11/env/../lib/intel64/gcc4.8:/opt/intel/oneapi/mpi/2021.11/opt/mpi/libfabric/lib:/opt/intel/oneapi/mpi/2021.11/lib:/opt/intel/oneapi/mkl/2024.0/lib:/opt/intel/oneapi/dpl/2022.3/lib:/opt/intel/oneapi/debugger/2024.0/opt/debugger/lib:/opt/intel/oneapi/compiler/2024.0/opt/oclfpga/host/linux64/lib:/opt/intel/oneapi/compiler/2024.0/opt/compiler/lib:/opt/intel/oneapi/compiler/2024.0/lib
++ export CAPS_GLYPH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ export TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ TETGEN=/home/jenkins/util/tetgen/tetgen1.6.0
++ export 'SLUGS_START=firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/wvClient/wv.html &'
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/src'
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/LINUX64
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/LINUX64
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/STANALYZER.make
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/STANALYZER.make
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.h
cp -p ../include/egads.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads_dot.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads_dot.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.inc
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egads.inc
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsErrors.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsErrors.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTypes.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTypes.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/emp.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/emp.h
cp -p ../include/emp.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/emp.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/prm.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/prm.h
cp -p ../include/prm.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/prm.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.inc
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsserver.inc
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsss.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/wsss.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTris.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsTris.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineFit.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineFit.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineVels.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsSplineVels.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsf90.inc
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egadsf90.inc
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/Surreal/always_inline.h
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsIO.cpp -o ./egadsIO.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
	-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include -I../util \
	-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
	-o ./emp.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/evaluate.c -o ./evaluate.o
g++ -g  -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
	../util/rational.c -o ./rational.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
	../util/regQuads.c -o ./regQuads.o
g++ -g  -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1

SurrealD1_test_suite Complete!

g++ -g  -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4

SurrealD4_test_suite Complete!

g++ -g  -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1

SurrealS1_test_suite Complete!

g++ -g  -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with ‘-fvar-tracking-assignments’, retrying without
 1265 | BOOST_AUTO_TEST_CASE( multiply_deriv2 )
      |                       ^~~~~~~~~~~~~~~
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
   19 | #define BOOST_AUTO_TEST_CASE( fun ) void fun()
      |                                          ^~~
./SurrealS4

SurrealS4_test_suite Complete!

make -C ../util
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/util'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 uvmap/main/uvmap.c -Iuvmap \
	-o ./uvmap.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
	-o ./egadsUVmap.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libuvmap.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o EG_uvmapFindUV.o EG_uvmapGen.o EG_uvmap_Read.o EG_uvmapStructFree.o EG_uvmapTest.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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libuvmap.a
gcc -g  -o ./uvmap.exe ./uvmap.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/util'
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegads.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegads.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegads.so \
	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 \
	-L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadstatic.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadstatic.a
cp /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libuvmap.a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadstatic.a
(cd .; \
	ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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;  )
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libfgads.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libfgads.a
(cd .; ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o  fgadsTess.o   fgadsHLevel.o fgadsGeom.o fgadsTopo.o;  )
ar: creating /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libfgads.a
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libemp.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libemp.a
(cd .; ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libemp.a emp.o;  )
ar: creating /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libemp.a
 *** EGADS Build Complete! ***
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/lite'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteBase.c -o ./liteBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteMemory.c -o ./liteMemory.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteGeom.c -o ./liteGeom.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteTopo.c -o ./liteTopo.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteAttrs.c -o ./liteAttrs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteImport.c -o ./liteImport.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
	liteString.c -o ./liteString.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTess.c -o ./liteTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsTris.c -o ./liteTris.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
                ../src/egadsQuads.c -o ./liteQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \
	-o ./egadsRobust.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \
	-o ./emp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
	../util/evaluate.c -o ./evaLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
	-o ./ratLite.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
	../util/regQuads.c -o ./liteRegQuads.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                ../src/egadsEffect.c -o ./liteEffect.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
                -I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslite.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g  -shared -Wl,-no-undefined \
	-o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslite.so 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 \
	-lpthread -lm )
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslitestatic.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/wvServer'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 map.cpp -o ./map.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include base64-decode.c -o ./base64-decode.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include handshake.c -o ./handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include client-handshake.c -o ./client-handshake.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include libwebsockets.c -o ./libwebsockets.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include extension-deflate-stream.c -o ./extension-deflate-stream.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include md5.c -o ./md5.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include extension-x-google-mux.c -o ./extension-x-google-mux.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include parsers.c -o ./parsers.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include extension.c -o ./extension.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include sha-1.c -o ./sha-1.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include server.c -o ./server.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include wv.c -o ./wv.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include browserMessage.c -o ./browserMessage.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include fwv.c -o ./fwv.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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 \
	./fwv.o;  )
ar: creating /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DLWS_NO_FORK -DSTANDALONE server.c \
	-I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -o ./servertest.o
g++ -g  -o ./server ./servertest.o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.a  \
	-lpthread -lz -lm
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g  -shared -Wl,-no-undefined \
	-o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libwsserver.so 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 -lpthread)
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include egads2cart.c \
	-o ./egads2cart.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/egads2cart ./egads2cart.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -legads \
	-lrt -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/vCurvature ./vCurvature.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/vGeom ./vGeom.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lwsserver -legads \
	-lrt
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include vTess.c -o ./vTess.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include ../util/retessFaces.c \
	-o ./retessFaces.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
	-lpthread -lz -lrt -lm
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. serveCSM.c -o ./serveCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. OpenCSM.c -o ./OpenCSM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udp.c -o ./udp.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. tim.c -o ./tim.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libocsm.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libocsm.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/serveCSM ./serveCSM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/serveESP ./serveESP.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/sensCSM ./sensCSM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bezier.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bezier.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bezier.so ./udpBezier.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/biconvex.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/biconvex.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/box.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/box.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/box.so ./udpBox.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bspline.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bspline.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bspline.so ./udpBspline.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/catmull.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/catmull.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/compare.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/compare.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/compare.so ./udfCompare.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createBEM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createBEM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createPoly.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createPoly.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/csm.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/csm.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/csm.so ./udpCsm.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/deform.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/deform.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/deform.so ./udfDeform.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/droop.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/droop.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/droop.so ./udfDroop.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/dumpPmtrs.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/dumpPmtrs.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/editAttr.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/editAttr.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ellipse.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ellipse.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/eqn2body.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/eqn2body.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/fitcurve.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/fitcurve.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flend.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flend.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flend.so ./udfFlend.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/freeform.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/freeform.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ganged.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ganged.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ganged.so ./udfGanged.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/guide.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/guide.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/guide.so ./udfGuide.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hex.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hex.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hex.so ./udpHex.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/import.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/import.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/import.so ./udpImport.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/kulfan.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/kulfan.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/linalg.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/linalg.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/matchBodys.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/matchBodys.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mechanism.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mechanism.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca.so ./udpNaca.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca6mc.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca6mc.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nacelle.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nacelle.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nurbbody.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nurbbody.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nuscale.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nuscale.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/offset.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/offset.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/offset.so ./udfOffset.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parabaloid.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parabaloid.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parsec.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parsec.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/parsec.so ./udpParsec.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pod.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pod.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pod.so ./udpPod.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/poly.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/poly.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/poly.so ./udpPoly.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBbox.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBbox.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBrep.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBrep.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printEgo.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printEgo.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/prop.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/prop.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/prop.so ./udpProp.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/radwaf.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/radwaf.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sample.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sample.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sample.so ./udpSample.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sew.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sew.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sew.so ./udpSew.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/shadow.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/shadow.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/shadow.so ./udfShadow.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slices.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slices.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slices.so ./udfSlices.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stag.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stag.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stag.so ./udpStag.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stiffener.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stiffener.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/supell.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/supell.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/supell.so ./udpSupell.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester1.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester1.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester1.so ./udfTester1.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester2.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester2.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tester2.so ./udpTester2.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vsp3.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vsp3.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/waffle.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/waffle.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/warp.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/warp.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/warp.so ./udfWarp.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/PDT2.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/PDT2.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -legads -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
ifort -g -traceback -c -O -fPIC -recursive naca456.f90 -o ./naca456.o -module .
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca456.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca456.so
ifort -g -traceback -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads -lm 
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ereped.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ereped.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ereped.so ./timEreped.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mitten.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mitten.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mitten.so ./timMitten.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plotter.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plotter.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plotter.so ./timPlotter.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plugs.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plugs.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/plugs.so ./timPlugs.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lrt
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slugs.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slugs.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/slugs.so ./timSlugs.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vspSetup.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vspSetup.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/OpenCSM.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/OpenCSM.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/common.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/common.h
cp -p common.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/common.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udp.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udp.h
cp -p udp.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udp.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/esp.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/esp.h
cp -p esp.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/esp.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/tim.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/tim.h
cp -p tim.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/tim.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egg.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egg.h
cp -p egg.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/egg.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.c
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/Slugs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. Slugs.c -o ./Slugs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. Fitter.c \
	-o ./Fitter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. RedBlackTree.c \
	-o ./RedBlackTree.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. Tessellate.c \
	-o ./Tessellate.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
	./Tessellate.o -lrt -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lwsserver -legads \
	-lpthread -lz -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -legads \
	-lpthread -lz -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/mset
/bin/cp Libraries/LINUX64/aflr2AIM.so /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/src'
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/caps.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/caps.h
cp -p ../include/caps.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/caps.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsErrors.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsErrors.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsTypes.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/capsTypes.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimUtil.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimUtil.h
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimMesh.h
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aimMesh.h
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../include \
	-I/usr/include/udunits2 aimUtil.c -o ./aimUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include \
	-I/usr/include/udunits2 aimTransferUtil.c \
	-o ./aimTransferUtil.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../include \
	aimMesh.c -o ./aimMesh.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libaimUtil.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libaimUtil.a
ar -rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
	./aimTransferUtil.o 
ar: creating /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libaimUtil.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBase.c -o ./capsBase.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAnalysis.c -o ./capsAnalysis.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsApprox.c -o ./capsApprox.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAttr.c -o ./capsAttr.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsAIM.c -o ./capsAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsBound.c -o ./capsBound.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsProblem.c -o ./capsProblem.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsValue.c -o ./capsValue.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsUnits.c -o ./capsUnits.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 conjGrad.c -o ./conjGrad.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsFunIDs.c -o ./capsFunIDs.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 capsChkInpt.c -o ./capsChkInpt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. \
	-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcaps.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcaps.so
(cd .; gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcaps.so \
		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 -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
		-lrt -lm )
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcapsstatic.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libcapsstatic.a
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include testingAIM.c \
	-o ./testingAIM.o
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingAIM.so
rm: cannot remove '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingAIM.so': No such file or directory
make[1]: [Makefile:23: /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include testingWriter.c \
	-o ./testingWriter.o
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingWriter.so
rm: cannot remove '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingWriter.so': No such file or directory
make[1]: [Makefile:33: /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -ldl -lrt -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include phaseUtil.c \
	-o ./phaseUtil.o
gcc -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include aeroelasticSimple_Iterative_SU2_and_MystranTest.c -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o
gcc -g  -o ./aeroelasticSimple_Iterative_SU2_and_MystranTest ./aeroelasticSimple_Iterative_SU2_and_MystranTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g  -o ./avlTest ./avlTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g  -o ./awaveTest ./awaveTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g  -o ./frictionTest ./frictionTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g  -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g  -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g  -o ./aeroelasticTest ./aeroelasticTest.o \
-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include hsmTest.c -o ./hsmTest.o   
gcc -g  -o ./hsmTest ./hsmTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o  
gcc -g  -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o  
gcc -g  -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o  
gcc -g  -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include interferenceTest.c \
	-o ./interferenceTest.o   
gcc -g  -o ./interferenceTest ./interferenceTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g  -o ./msesTest ./msesTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -legads -locsm \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include mystranTest.c -o ./mystranTest.o   
gcc -g  -o ./mystranTest ./mystranTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g  -o ./pointwiseTest ./pointwiseTest.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads \
	-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/utils'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython attrUtils.c -o ./attrUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython meshUtils.c -o ./meshUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cfdUtils.c -o ./cfdUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython miscUtils.c -o ./miscUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython feaUtils.c -o ./feaUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython vlmUtils.c -o ./vlmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranCards.c -o ./nastranCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython nastranUtils.c -o ./nastranUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython tecplotUtils.c -o ./tecplotUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython arrayUtils.c -o ./arrayUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython deprecateUtils.c -o ./deprecateUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cardUtils.c -o ./cardUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython jsonUtils.c -o ./jsonUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython cython/nastranOP2Reader.c -o ./nastranOP2Reader.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libutils.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libutils.a
(cd .; ar -rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libutils.a
mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils
cp -p -f arrayUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f attrTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f attrUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f cardTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f cardUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/cardUtils.h
cp -p -f cfdTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f cfdUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f deprecateUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f feaTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f feaUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f jsonUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f meshTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f meshUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f miscTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f miscUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f nastranCards.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f nastranUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f tecplotUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f vlmTypes.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f vlmUtils.h /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/aim/utils/vlmUtils.h
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/utils'
make -C abaqus 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/abaqus'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	abaqusAIM.c -o ./abaqusAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	abaqusUtils.c -o ./abaqusUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/abaqusFILReader.c -o ./abaqusFILReader.o
echo "Building Abaqus with Python"
Building Abaqus with Python
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -ldl -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/abaqus'
make -C aflr2 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr3 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr3'
make -C aflr4 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/aflr4'
make -C astros 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/astros'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils astrosAIM.c \
	-o ./astrosAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils astrosUtils.c \
	-o ./astrosUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils astrosCards.c \
        -o ./astrosCards.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o  ./astrosUtils.o ./astrosCards.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/astros'
make -C avl 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/avl'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils avlAIM.c -o ./avlAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_BODY.c -o avlRead_BODY.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CNC.c -o avlRead_CNC.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_CPOML.c -o avlRead_CPOML.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATB.c -o avlRead_DERMATB.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATM.c -o avlRead_DERMATM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_DERMATS.c -o avlRead_DERMATS.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_ELE.c -o avlRead_ELE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_HINGE.c -o avlRead_HINGE.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_STRP.c -o avlRead_STRP.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_SURF.c -o avlRead_SURF.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_TOT.c -o avlRead_TOT.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -Wno-unused-function -Iavlmrf avlmrf/avlRead_VM.c -o avlRead_VM.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/avlAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/avlAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_CPOML.o ./avlRead_DERMATB.o ./avlRead_DERMATM.o ./avlRead_DERMATS.o ./avlRead_ELE.o ./avlRead_HINGE.o ./avlRead_STRP.o ./avlRead_SURF.o ./avlRead_TOT.o ./avlRead_VM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
	-lstdc++ -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/avl'
make -C awave 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/awave'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils awaveAIM.c \
	-o ./awaveAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/awave'
make -C cart3d 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cart3d'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCAPS_MESHUTILS -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/libCart3D -I./xddm \
	cart3dAIM.c -o ./cart3dAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/c3dio \
	-I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/libCart3D -I./xddm \
	writeTrix.c -o ./writeTrix.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/c3dio \
	-I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/libCart3D \
	surfTrix.c -o ./surfTrix.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -pedantic -I./xddm -I. \
	`xml2-config --cflags` ./xddm/xddm.c \
	 -o ./xddm.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include bodyTess.c -o ./bodyTess.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/cart3dAIM.so ./cart3dAIM.o \
	./writeTrix.o ./surfTrix.o ./xddm.o ./bodyTess.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils \
	-laimUtil -locsm -legads -ludunits2 -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/ \
	-lc3dio -lCart3D -ldl -lxml2 -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include cart3dTest.c \
	-o ./cart3dTest.o
gcc -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/cart3dTest ./cart3dTest.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -legads -lrt -lm -ldl
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I./xddm \
	-I. `xml2-config --cflags` ESPxddm.c -o ./ESPxddm.o
gcc -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/ESPxddm ./ESPxddm.o ./writeTrix.o \
	./surfTrix.o ./xddm.o ./bodyTess.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -locsm -legads \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include/ -lc3dio -lCart3D \
	-lpthread -ldl  -lxml2 -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cart3d'
make -C cbaero 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cbaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g  -shared -Wl,-no-undefined  cbaeroAIM.o -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/cbaeroAIM.so -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cbaero'
make -C cgt 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cgt'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include egads2cgt.c \
	-o ./egads2cgt.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include aflr4egads.c \
	-o ./aflr4egads.o
g++ -g  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/cgt'
make -C custom 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for 'default'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/custom'
make -C delaundo 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/delaundo'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils delaundoAIM.c \
	-o ./delaundoAIM.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/delaundoAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/delaundoAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/delaundo'
make -C egadsTess 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/egadsTess'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils egadsTessAIM.c \
	-o ./egadsTessAIM.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/egadsTessAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/egadsTessAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/egadsTess'
make -C friction 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/friction'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -Wno-format -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils frictionAIM.c \
	-o ./frictionAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
ifort -g -traceback -c -O -fPIC -recursive friction_eja_mod.f -o ./friction.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
ifort -g -traceback -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin/friction ./friction.o 
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/friction'
make -C fun3d 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/fun3d'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython fun3dAIM.c -o ./fun3dAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils -I../meshWriter/ugridWriter \
	fun3dUtils.c -o ./fun3dUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
	-I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	-I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 cython/fun3dNamelist.c -o ./fun3dNamelist.o
Building FUN3D with Python
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
	./fun3dNamelist.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -lm -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/fun3d'
make -C hsm 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils hsmAIM.c \
	-o src/hsmAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils hsmUtils.c \
	-o src/hsmUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils hsmAdj.c \
	-o src/hsmAdj.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -Wno-comment rcm/rcm.cpp -DREVISION=7.8 \
	-o src/rcm.o
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
	-o src/genrcmi.o
make -C src atanc.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   atanc.f -o ./atanc.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   bmdump.f -o ./bmdump.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   cross.f -o ./cross.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmabd.f -o ./hsmabd.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmbb2.f -o ./hsmbb2.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmbc.f -o ./hsmbc.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmdep.f -o ./hsmdep.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmeqn.f -o ./hsmeqn.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmgeo.f -o ./hsmgeo.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmglr.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmglr.f -o ./hsmglr.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmout.f -o ./hsmout.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmprj.f -o ./hsmprj.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmre1.f -o ./hsmre1.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmren.f -o ./hsmren.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmrfm.f -o ./hsmrfm.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds  -norecursive hsmrun.f -o ./hsmrun.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   hsmsol.f -o ./hsmsol.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   ludcmp.f -o ./ludcmp.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
ifort -g -traceback -c -O -fPIC -recursive -real-size 64 -check bounds   sbsolve.f -o ./sbsolve.o
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libhsm.a
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libhsm.a
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm/src'
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hsmAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hsmAIM.so
ifort -g -traceback -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/hsmAIM.so \
	src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
	src/rcm.o src/genrcmi.o \
	 -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -lhsm -ldl  -lstdc++ 
ifort: remark #10448: Intel(R) Fortran Compiler Classic (ifort) is now deprecated and will be discontinued late 2024. Intel recommends that customers transition now to using the LLVM-based Intel(R) Fortran Compiler (ifx) for continued Windows* and Linux* support, new language support, new language features, and optimizations. Use '-diag-disable=10448' to disable this message.
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/hsm'
make -C interference 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/interference'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include interferenceAIM.c \
	-o ./interferenceAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. cloudFns.c \
	-o ./cloudFns.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/interferenceAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/interferenceAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/interferenceAIM.so \
	./interferenceAIM.o ./cloudFns.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib \
	-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/interference'
make -C masstran 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/masstran'
g++ -g  -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils masstranAIM.cpp \
	-o ./masstranAIM.o
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/masstran'
make -C meshWriter 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter'
make -C bstlWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include bstlWriter.c \
	-o ./bstlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include bvtkWriter.c \
	-o ./bvtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C exodusWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8  -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I/home/jenkins/util/sandialabs/seacas/include -I. exodusWriter.cpp \
	-o ./exodusWriter.o
g++ -g  -shared -Wl,-no-undefined  -std=c++11 -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/exodusWriter.so ./exodusWriter.o \
	-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib  -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make -C fastWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include fastWriter.c \
	-o ./fastWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C libmeshbWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include libmeshbWriter.c \
	-o ./libmeshbWriter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8  -IlibMeshb/sources -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C stlWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include stlWriter.c \
	-o ./stlWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C su2Writer 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include su2Writer.c \
	-o ./su2Writer.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C tecplotWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include tecplotWriter.c \
	-o ./tecplotWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C ugridWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include ugridWriter.c \
	-o ./ugridWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C vtkWriter 
make[3]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include vtkWriter.c \
	-o ./vtkWriter.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/meshWriter'
make -C mses 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/mses'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils msesAIM.c -o msesAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/mses'
make -C mystran 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/mystran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils mystranAIM.c \
	-o ./mystranAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils mystranUtils.c \
	-o ./mystranUtils.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/mystran'
make -C nastran 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/nastran'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils nastranAIM.c \
	-o ./nastranAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/nastran'
make -C plato 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/plato'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/home/jenkins/util/sandialabs/seacas/include -I. platoAIM.c \
	-o ./platoAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/platoAIM.so ./platoAIM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib \
	-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib  \
	-laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/plato'
make -C pointwise 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils pointwiseAIM.c \
	-o ./pointwiseAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils hashElement.c \
	-o ./hashElement.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pointwiseAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pointwiseAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm -lpthread
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise'
make -C refine 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/refine'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils -I../meshWriter/libmeshbWriter refineAIM.c \
	-o ./refineAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \
	-I../meshWriter/libmeshbWriter/libMeshb/sources \
	../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/refineAIM.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/refineAIM.so
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
	-lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/refine'
make -C sierraSD 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/sierraSD'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/home/jenkins/util/sandialabs/seacas/include -I. sierraSDAIM.c \
	-o ./sierraSDAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sierraSDAIM.so ./sierraSDAIM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib \
	-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib  \
	-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/sierraSD'
make -C sierraSM 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/sierraSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../meshWriter/exodusWriter -I../utils  -I/home/jenkins/util/sandialabs/seacas/include -I. sierraSMAIM.c \
	-o ./sierraSMAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/sierraSMAIM.so ./sierraSMAIM.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib \
	-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib  \
	-lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/sierraSM'
make -C skeleton 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/skeleton'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils skeletonAIM.c \
	-o ./skeletonAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/skeleton'
make -C spinnaker 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/spinnaker'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include \
	-I../meshWriter/exodusWriter \
	-I../meshWriter/libmeshbWriter \
	-I../utils -I/home/jenkins/util/sandialabs/seacas/include \
	-I. \
	spinnakerAIM.c \
	-o ./spinnakerAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 \
	-I../meshWriter/libmeshbWriter/libMeshb/sources \
	../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
	-o ./libmeshb7.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/spinnakerAIM.so ./spinnakerAIM.o ./libmeshb7.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib \
	-L/home/jenkins/util/sandialabs/seacas/lib -lexodus -Wl,-rpath /home/jenkins/util/sandialabs/seacas/lib  \
	-laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/spinnaker'
make -C su2 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/su2'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../meshWriter/su2Writer -I../utils su2AIM.c \
	-o ./su2AIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2Utils.c \
	-o ./su2Utils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2_4_Cardinal.c \
	-o ./su2_4_Cardinal.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2_5_Raven.c \
	-o ./su2_5_Raven.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2_6_Falcon.c \
	-o ./su2_6_Falcon.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2_7_Blackbird.c \
	-o ./su2_7_Blackbird.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils su2_801_Harrier.c \
	-o ./su2_801_Harrier.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/su2AIM.so ./su2AIM.o ./su2Utils.o ./su2_4_Cardinal.o ./su2_5_Raven.o ./su2_6_Falcon.o ./su2_7_Blackbird.o ./su2_801_Harrier.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/su2'
make -C tacs 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tacs'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils tacsAIM.c \
	-o ./tacsAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tacs'
make -C tetgen 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tetgen'
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils tetgenAIM.cpp \
	-o ./tetgenAIM.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I/home/jenkins/util/tetgen/tetgen1.6.0 -I../utils \
	-DTETLIBRARY tetgen_Interface.cpp -o ./tetgen_Interface.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DTETLIBRARY -w /home/jenkins/util/tetgen/tetgen1.6.0/tetgen.cxx -o ./tetgen.o
g++ -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -O0 -w /home/jenkins/util/tetgen/tetgen1.6.0/predicates.cxx -o ./predicates.o
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
	./tetgen_Interface.o ./tetgen.o \
	./predicates.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm \
	-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tetgen'
make -C tsfoil 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tsfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/tsfoil'
make -C unitTest 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for 'all'.
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest'
make -C xfoil 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/xfoil'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils \
	xfoilAIM.c -o ./xfoilAIM.o
gcc -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
	-L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/xfoil'
make -C zaero 
make[2]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/zaero'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroAIM.c -o zaeroAIM.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroUtils.c -o zaeroUtils.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroLinearFlutter.c -o zaeroLinearFlutter.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroTrim.c -o zaeroTrim.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroTypes.c -o zaeroTypes.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroCards.c -o zaeroCards.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroGeneral.c -o zaeroGeneral.o
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g  -shared -Wl,-no-undefined   -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/OpenCSM'
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/capsMode.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/capsMode.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flowchart.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flowchart.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/viewer.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/viewer.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/viewer.so ./timViewer.o -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lm
gcc -g  -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pyscript.so
rm /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pyscript.so
g++ -g  -shared -Wl,-no-undefined  -o /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/lib -lcaps -locsm -lwsserver -legads -ldl -lrt -Wl,-rpath /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/OpenCSM'
 
 *** Build Completed! ***
+ export CSMDATA=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data
+ CSMDATA=/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds 6.5.0-18-generic #18~22.04.1-Ubuntu SMP PREEMPT_DYNAMIC Wed Feb  7 11:40:03 UTC 2 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]]
+ sed -i 's/.*capsExamples.*/#&/' /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/Verification.sh
+ bash -ex /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/Verification.sh
+ expectSuccess 01 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data

real	0m0.067s
user	0m0.054s
sys	0m0.012s
+ set +x

=============================================
ESP verification case 01 passed (as expected)
=============================================

+ expectSuccess 02 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.352s
user	0m0.446s
sys	0m0.045s
+ set +x

=============================================
ESP verification case 02 passed (as expected)
=============================================

+ expectSuccess 03 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m3.113s
user	0m4.648s
sys	0m2.059s
+ set +x

=============================================
ESP verification case 03 passed (as expected)
=============================================

+ expectSuccess 04 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/design2
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.462s
user	0m0.656s
sys	0m0.052s
+ set +x

=============================================
ESP verification case 04 passed (as expected)
=============================================

+ expectSuccess 05 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/design3
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.381s
user	0m0.747s
sys	0m0.600s
+ set +x

=============================================
ESP verification case 05 passed (as expected)
=============================================

+ expectSuccess 06 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.410s
user	0m0.853s
sys	0m0.480s
+ set +x

=============================================
ESP verification case 06 passed (as expected)
=============================================

+ expectSuccess 07 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m6.022s
user	0m8.417s
sys	0m7.634s
+ set +x

=============================================
ESP verification case 07 passed (as expected)
=============================================

+ expectSuccess 08 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data

real	0m24.465s
user	0m51.033s
sys	0m33.852s
+ set +x

=============================================
ESP verification case 08 passed (as expected)
=============================================

+ expectSuccess 09 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/bottle
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.569s
user	0m0.890s
sys	0m0.020s
+ set +x

=============================================
ESP verification case 09 passed (as expected)
=============================================

+ expectSuccess 10 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data

real	0m29.542s
user	1m59.091s
sys	6m15.326s
+ set +x

=============================================
ESP verification case 10 passed (as expected)
=============================================

+ expectSuccess 11 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: could not find mapping for iedge=10
WARNING:: could not find mapping for iedge=14
WARNING:: could not find mapping for iedge=7
WARNING:: could not find mapping for iedge=11
==> serveESP completed successfully with 5 warnings and no verification data

real	0m0.218s
user	0m0.261s
sys	0m0.071s
+ set +x

=============================================
ESP verification case 11 passed (as expected)
=============================================

+ expectSuccess 12 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.409s
user	0m0.645s
sys	0m0.020s
+ set +x

=============================================
ESP verification case 12 passed (as expected)
=============================================

+ expectSuccess 13 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/group2
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data

real	0m0.111s
user	0m0.163s
sys	0m0.013s
+ set +x

=============================================
ESP verification case 13 passed (as expected)
=============================================

+ expectSuccess 14 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data

real	0m0.250s
user	0m0.392s
sys	0m0.017s
+ set +x

=============================================
ESP verification case 14 passed (as expected)
=============================================

+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/pyESP/testEGADS
+ make test
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 71 tests in 1.933s

OK
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/pyESP/testOCSM
+ source /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp

real	0m4.531s
user	0m9.216s
sys	0m0.200s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/pyESP/testCAPS
+ make 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 = 140
	Number of elements = 276
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 276
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 283
	Combined Number of elements = 558
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 558
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
..Writing D3 Javascript library -  d3.v3.min.js
........... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.No analysis directory provided - defaulting to altName
Mapping Csys attributes ................
	Number of unique Csys attributes = 2
	Name = leftWingSkin, index = 1
	Name = riteWingSkin, index = 2

Getting FEA coordinate systems.......
	Number of coordinate systems - 2
	Coordinate system name - leftWingSkin
	Coordinate system name - riteWingSkin
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Upper_Left, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing1, index = 1
	Name = Wing2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 209
	Number of elements = 414
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 414
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 186
	Number of elements = 368
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 368
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 395
	Combined Number of elements = 782
	Combined Elemental Nodes = 0
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 782
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - Wing1
	Property name - Wing2
	Done getting FEA properties
Updating mesh element types based on properties input
..........--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
..Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
No linkable data found for Altitude
No linkable data found for Strings
No linkable data found for Strings2
Linked Parameter Beta to analysis su2 input Beta
Linked Parameter Alpha to analysis su2 input Alpha
............ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. CAPS Info: Hit last success -- going live!
... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> _body (EG_attributeDel)!
 EGADS Error: No Attribute -> _nface (EG_attributeDel)!
 EGADS Error: No Attribute -> __trace__ (EG_attributeDel)!
 EGADS Error: No Attribute -> __numRemaining__ (EG_attributeDel)!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
.--> Opening DESPMTR file "unitGeom.param"
    updating CFGPMTR series                          [ 1, 1] =  8412.000000
    updating CFGPMTR series2                         [ 1, 1] =    20.000000
    updating CFGPMTR VIEW:CFD                        [ 1, 1] =     1.000000
    updating CFGPMTR nrow                            [ 1, 1] =     3.000000
    updating CFGPMTR ncol                            [ 1, 1] =     2.000000
    updating DESPMTR area                            [ 1, 1] =    40.000000
    updating DESPMTR aspect                          [ 1, 1] =     5.000000
    updating DESPMTR taper                           [ 1, 1] =     0.500000
    updating DESPMTR twist                           [ 1, 1] =    15.000000
    updating DESPMTR wing:lesweep                    [ 1, 1] =    30.000000
    updating DESPMTR wing:dihedral                   [ 1, 1] =     1.000000
    updating DESPMTR wing:chord:root                 [ 1, 1] =     1.560000
    updating DESPMTR htail                           [ 1, 1] =     1.000000
    updating DESPMTR htail:chord                     [ 1, 1] =     2.000000
    updating DESPMTR vtail:chord                     [ 1, 1] =     3.000000
    updating DESPMTR vtail                           [ 1, 1] =     4.000000
    updating DESPMTR sphereR                         [ 1, 1] =    80.000000
    updating DESPMTR v@1:d_name                      [ 1, 1] =     1.000000
    updating DESPMTR despMat                         [ 1, 1] =    11.000000
    updating DESPMTR despMat                         [ 1, 2] =    12.000000
    updating DESPMTR despMat                         [ 2, 1] =    13.000000
    updating DESPMTR despMat                         [ 2, 2] =    14.000000
    updating DESPMTR despMat                         [ 3, 1] =    15.000000
    updating DESPMTR despMat                         [ 3, 2] =    16.000000
    updating DESPMTR despCol                         [ 1, 1] =    11.000000
    updating DESPMTR despCol                         [ 2, 1] =    13.000000
    updating DESPMTR despCol                         [ 3, 1] =    15.000000
    updating DESPMTR despRow                         [ 1, 1] =    11.000000
    updating DESPMTR despRow                         [ 1, 2] =    12.000000
    updating DESPMTR despRow                         [ 1, 3] =    13.000000
ERROR:: DESPMTR file "unitGeom.param" not found
 CAPS Error: ocsmSaveDespmtrs = -201 (caps_readParameters)!
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
. EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
................ EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!

----------------------------------------------------------------------
Ran 100 tests in 9.743s

OK
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/
+ make test
python --version
Python 3.11.9
python -u -m unittest discover --verbose
Please set the environment variable ASTROS_ROOT
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
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          =     0.029   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.091   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =      2224         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =      2224      2224
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       446       894
AFLR2 IG : Nodes, Faces      =       892      1786
AFLR2 IG : Nodes, Faces      =       918      1838
AFLR2 IG : Nodes, Faces      =      1033      2068
AFLR2 IG : Nodes, Faces      =      1133      2268
AFLR2 IG : Nodes, Faces      =      1233      2468
AFLR2 IG : Nodes, Faces      =      1333      2668
AFLR2 IG : Nodes, Faces      =      1338      2678
AFLR2 IG : Nodes, Faces      =      1433      2868
AFLR2 IG : Nodes, Faces      =      1533      3068
AFLR2 IG : Nodes, Faces      =      1633      3268
AFLR2 IG : Nodes, Faces      =      1733      3468
AFLR2 IG : Nodes, Faces      =      1784      3570
AFLR2 IG : Nodes, Faces      =      1833      3668
AFLR2 IG : Nodes, Faces      =      1858      3718
AFLR2 IG : Nodes, Faces      =      2224      4450
AFLR2 IG : Nodes, Faces      =      2228      4450
AFLR2 IG : Nodes, Faces      =      2224      2224
 
AFLR2    : CPU Time          =     0.034   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.108   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.008   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 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      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.089   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.007   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 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          =     0.035   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2224      2224
AFLR2 GG : Nodes, Faces      =      4122      6020
AFLR2 GG : Nodes, Faces      =      5812      9400
AFLR2 GG : Nodes, Faces      =      7299     12374
AFLR2 GG : Nodes, Faces      =      8574     14924
AFLR2 GG : Nodes, Faces      =      9729     17234
AFLR2 GG : Nodes, Faces      =     10787     19350
AFLR2 GG : Nodes, Faces      =     11767     21310
AFLR2 GG : Nodes, Faces      =     12683     23142
AFLR2 GG : Nodes, Faces      =     13516     24808
AFLR2 GG : Nodes, Faces      =     14278     26332
AFLR2 GG : Nodes, Faces      =     14999     27774
AFLR2 GG : Nodes, Faces      =     15682     29140
AFLR2 GG : Nodes, Faces      =     16312     30400
AFLR2 GG : Nodes, Faces      =     16899     31574
AFLR2 GG : Nodes, Faces      =     17451     32678
AFLR2 GG : Nodes, Faces      =     17959     33694
AFLR2 GG : Nodes, Faces      =     18443     34662
AFLR2 GG : Nodes, Faces      =     18877     35530
AFLR2 GG : Nodes, Faces      =     19283     36342
AFLR2 GG : Nodes, Faces      =     19650     37076
AFLR2 GG : Nodes, Faces      =     19994     37764
AFLR2 GG : Nodes, Faces      =     20325     38426
AFLR2 GG : Nodes, Faces      =     20638     39052
AFLR2 GG : Nodes, Faces      =     20940     39656
AFLR2 GG : Nodes, Faces      =     21240     40256
AFLR2 GG : Nodes, Faces      =     21523     40822
AFLR2 GG : Nodes, Faces      =     21792     41360
AFLR2 GG : Nodes, Faces      =     22053     41882
AFLR2 GG : Nodes, Faces      =     22305     42386
AFLR2 GG : Nodes, Faces      =     22521     42818
AFLR2 GG : Nodes, Faces      =     22696     43168
AFLR2 GG : Nodes, Faces      =     22829     43434
AFLR2 GG : Nodes, Faces      =     22953     43682
AFLR2 GG : Nodes, Faces      =     23050     43876
AFLR2 GG : Nodes, Faces      =     23110     43996
AFLR2 GG : Nodes, Faces      =     23139     44054
AFLR2 GG : Nodes, Faces      =     23157     44090
AFLR2 GG : Nodes, Faces      =     23175     44126
AFLR2 GG : Nodes, Faces      =     23183     44142
AFLR2 GG : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.137   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     23187     44150
 
AFLR2    : CPU Time          =     0.040   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
 CAPS Info: Hit last success -- going live!
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
ok
test_phase (test_aflr2.TestAFLR2.test_phase) ... Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 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          =     0.042   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =      2244      2244
AFLR2 GG : Nodes, Faces      =      4283      6322
AFLR2 GG : Nodes, Faces      =      6128     10012
AFLR2 GG : Nodes, Faces      =      7863     13482
AFLR2 GG : Nodes, Faces      =      9464     16684
AFLR2 GG : Nodes, Faces      =     10948     19652
AFLR2 GG : Nodes, Faces      =     12322     22400
AFLR2 GG : Nodes, Faces      =     13619     24994
AFLR2 GG : Nodes, Faces      =     14829     27414
AFLR2 GG : Nodes, Faces      =     15981     29718
AFLR2 GG : Nodes, Faces      =     17082     31920
AFLR2 GG : Nodes, Faces      =     18110     33976
AFLR2 GG : Nodes, Faces      =     19081     35918
AFLR2 GG : Nodes, Faces      =     20014     37784
AFLR2 GG : Nodes, Faces      =     20924     39604
AFLR2 GG : Nodes, Faces      =     21782     41320
AFLR2 GG : Nodes, Faces      =     22595     42946
AFLR2 GG : Nodes, Faces      =     23377     44510
AFLR2 GG : Nodes, Faces      =     24129     46014
AFLR2 GG : Nodes, Faces      =     24840     47436
AFLR2 GG : Nodes, Faces      =     25522     48800
AFLR2 GG : Nodes, Faces      =     26170     50096
AFLR2 GG : Nodes, Faces      =     26793     51342
AFLR2 GG : Nodes, Faces      =     27346     52448
AFLR2 GG : Nodes, Faces      =     27846     53448
AFLR2 GG : Nodes, Faces      =     28280     54316
AFLR2 GG : Nodes, Faces      =     28652     55060
AFLR2 GG : Nodes, Faces      =     28920     55596
AFLR2 GG : Nodes, Faces      =     29143     56042
AFLR2 GG : Nodes, Faces      =     29358     56472
AFLR2 GG : Nodes, Faces      =     29550     56856
AFLR2 GG : Nodes, Faces      =     29693     57142
AFLR2 GG : Nodes, Faces      =     29805     57366
AFLR2 GG : Nodes, Faces      =     29875     57506
AFLR2 GG : Nodes, Faces      =     29895     57546
AFLR2 GG : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.110   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     29897     57550
 
AFLR2    : CPU Time          =     0.010   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 29897
Number of elements = 59794
Number of tris = 57550
Number of quad = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 5
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = TunnelWall, index = 1
	Name = OutFlow, index = 2
	Name = InFlow, index = 3
	Name = Airfoil, index = 4
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =        48         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        10        22
AFLR2 IG : Nodes, Faces      =        20        42
AFLR2 IG : Nodes, Faces      =        30        62
AFLR2 IG : Nodes, Faces      =        40        82
AFLR2 IG : Nodes, Faces      =        45        92
AFLR2 IG : Nodes, Faces      =        46        94
AFLR2 IG : Nodes, Faces      =        48        98
AFLR2 IG : Nodes, Faces      =        52        98
AFLR2 IG : Nodes, Faces      =        48        48
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GG : Nodes, Faces      =        48        48
AFLR2 GG : Nodes, Faces      =        88       128
AFLR2 GG : Nodes, Faces      =       109       170
AFLR2 GG : Nodes, Faces      =       124       200
AFLR2 GG : Nodes, Faces      =       136       224
AFLR2 GG : Nodes, Faces      =       148       248
AFLR2 GG : Nodes, Faces      =       161       274
AFLR2 GG : Nodes, Faces      =       171       294
AFLR2 GG : Nodes, Faces      =       181       314
AFLR2 GG : Nodes, Faces      =       187       326
AFLR2 GG : Nodes, Faces      =       190       332
 
AFLR2    : CPU Time          =     0.001   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 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 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          =     0.015   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4705      9066
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Binary STL file ....
Finished writing Binary STL 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 vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file


Getting mesh sizing parameters
	Mesh sizing name - 2DSlice
	Mesh sizing name - Airfoil
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       344         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       344       344
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =        70       142
AFLR2 IG : Nodes, Faces      =       140       282
AFLR2 IG : Nodes, Faces      =       210       422
AFLR2 IG : Nodes, Faces      =       280       562
AFLR2 IG : Nodes, Faces      =       339       680
AFLR2 IG : Nodes, Faces      =       340       682
AFLR2 IG : Nodes, Faces      =       344       690
AFLR2 IG : Nodes, Faces      =       348       690
AFLR2 IG : Nodes, Faces      =       344       344
 
AFLR2    : CPU Time          =     0.001   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       344       344
AFLR2 GGp: Nodes, Faces      =       682      1020
AFLR2 GGp: Nodes, Faces      =      1010      1676
AFLR2 GGp: Nodes, Faces      =      1316      2288
AFLR2 GGp: Nodes, Faces      =      1592      2840
AFLR2 GGp: Nodes, Faces      =      1855      3366
AFLR2 GGp: Nodes, Faces      =      2106      3868
AFLR2 GGp: Nodes, Faces      =      2341      4338
AFLR2 GGp: Nodes, Faces      =      2551      4758
AFLR2 GGp: Nodes, Faces      =      2741      5138
AFLR2 GGp: Nodes, Faces      =      2917      5490
AFLR2 GGp: Nodes, Faces      =      3082      5820
AFLR2 GGp: Nodes, Faces      =      3240      6136
AFLR2 GGp: Nodes, Faces      =      3379      6414
AFLR2 GGp: Nodes, Faces      =      3513      6682
AFLR2 GGp: Nodes, Faces      =      3642      6940
AFLR2 GGp: Nodes, Faces      =      3748      7152
AFLR2 GGp: Nodes, Faces      =      3846      7348
AFLR2 GGp: Nodes, Faces      =      3931      7518
AFLR2 GGp: Nodes, Faces      =      3999      7654
AFLR2 GGp: Nodes, Faces      =      4044      7744
AFLR2 GGp: Nodes, Faces      =      4058      7772
 
AFLR2    : CPU Time          =     0.012   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
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Binary STL file ....
Finished writing Binary STL 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 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 vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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 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          =     0.010   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =      4058      7772
AFLR2 QI : Nodes, Faces      =      4057       364
AFLR2 QI : Nodes, Faces      =      4057      3703
AFLR2 QI : Nodes, Faces      =      4057      7770
AFLR2 QI : Nodes, Faces      =      4056       344
AFLR2 QI : Nodes, Faces      =      4056      3712
AFLR2 QI : Nodes, Faces      =      4056      7768
AFLR2 QI : Nodes, Faces      =      4055       348
AFLR2 QI : Nodes, Faces      =      4055      3709
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       392
AFLR2 QI : Nodes, Faces      =      4055      3687
AFLR2 QI : Nodes, Faces      =      4055      7766
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
AFLR2 QI : Nodes, Faces      =      4055       386
AFLR2 QI : Nodes, Faces      =      4055      3690
 
AFLR2    : CPU Time          =     0.006   seconds
 
AFLR2    : DONE

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 4055
Number of elements = 4420
Number of tris = 386
Number of quad = 3690

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_Multiple_Mesh (test_aflr3.TestAFLR3.test_Multiple_Mesh) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4    : Compile Date   04/23/24 @ 12:17PM
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          = 1189
	Number of elements       = 6249
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 6281
	Number of elements       = 34888
	Number of triangles      = 4448
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 30440
	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          = 13612
	Number of elements       = 76381
	Number of triangles      = 8144
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 68237
	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          = 41953
	Number of elements       = 238379
	Number of triangles      = 19880
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 218499
	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          = 4364
	Number of elements       = 24190
	Number of triangles      = 3016
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 21174
	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          = 11063
	Number of elements       = 61143
	Number of triangles      = 8630
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52513
	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          = 10571
	Number of elements       = 59256
	Number of triangles      = 6368
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 52888
	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          = 89033
	Number of elements       = 500486
	Number of triangles      = 51818
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 448668
	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:62408)
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

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          = 16433
	Number of elements       = 93529
	Number of triangles      = 7926
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 85603
	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          = 2589
	Number of elements       = 13809
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11051
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 3645
	Number of elements       = 19765
	Number of triangles      = 3394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 16371
	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          = 5471
	Number of elements       = 30418
	Number of triangles      = 3656
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 26762
	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          = 4694
	Number of elements       = 25935
	Number of triangles      = 3326
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22609
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 5554
	Number of elements       = 30862
	Number of triangles      = 3756
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 27106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 2260
	Number of elements       = 12133
	Number of triangles      = 2222
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 2392
	Number of elements       = 12577
	Number of triangles      = 2666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 9911
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 3341
	Number of elements       = 18069
	Number of triangles      = 3110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 3606
	Number of elements       = 18961
	Number of triangles      = 4002
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 14959
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 4414
	Number of elements       = 23974
	Number of triangles      = 3998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 4811
	Number of elements       = 25310
	Number of triangles      = 5334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19976
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 5490
	Number of elements       = 29891
	Number of triangles      = 4886
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 6019
	Number of elements       = 31671
	Number of triangles      = 6666
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25005
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 6542
	Number of elements       = 35667
	Number of triangles      = 5774
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7203
	Number of elements       = 37891
	Number of triangles      = 7998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 29893
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7601
	Number of elements       = 41489
	Number of triangles      = 6662
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 8394
	Number of elements       = 44157
	Number of triangles      = 9330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 34827
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 19800
	Number of elements       = 109798
	Number of triangles      = 15540
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 22741
	Number of elements       = 119570
	Number of triangles      = 25312
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94258
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6360
	Number of triangles      = 1334
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5026
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6217
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4885
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1214
	Number of elements       = 6384
	Number of triangles      = 1336
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5048
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1205
	Number of elements       = 6349
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5017
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1208
	Number of elements       = 6361
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5029
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6220
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4888
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1191
	Number of elements       = 6266
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4934
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1193
	Number of elements       = 6272
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4940
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1176
	Number of elements       = 6165
	Number of triangles      = 1330
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4835
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1203
	Number of elements       = 6314
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4982
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1192
	Number of elements       = 6269
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4937
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1198
	Number of elements       = 6296
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4964
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1223
	Number of elements       = 6443
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5111
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1184
	Number of elements       = 6224
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4892
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1195
	Number of elements       = 6287
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4955
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1197
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1203
	Number of elements       = 6310
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4978
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = wall, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1191
	Number of elements       = 6253
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4921
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 8857
	Number of elements       = 49191
	Number of triangles      = 6284
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 8989
	Number of elements       = 49635
	Number of triangles      = 6728
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 42907
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7796
	Number of elements       = 43368
	Number of triangles      = 5396
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 6267
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4935
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9944
	Number of elements       = 55193
	Number of triangles      = 7174
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 10218
	Number of elements       = 56081
	Number of triangles      = 8062
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 48019
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7818
	Number of elements       = 43469
	Number of triangles      = 5398
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38071
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1202
	Number of elements       = 6320
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4988
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1198
	Number of elements       = 6292
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4960
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9609
	Number of elements       = 53228
	Number of triangles      = 6994
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9829
	Number of elements       = 53956
	Number of triangles      = 7722
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 46234
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7789
	Number of elements       = 43295
	Number of triangles      = 5394
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37901
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1186
	Number of elements       = 6230
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4898
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 854
	Number of elements       = 4431
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3435
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9348
	Number of elements       = 51734
	Number of triangles      = 6812
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9531
	Number of elements       = 52330
	Number of triangles      = 7408
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44922
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7804
	Number of elements       = 43358
	Number of triangles      = 5386
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37972
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1200
	Number of elements       = 6311
	Number of triangles      = 1332
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4979
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9183
	Number of elements       = 50871
	Number of triangles      = 6632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 9322
	Number of elements       = 51307
	Number of triangles      = 7068
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 44239
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7927
	Number of elements       = 44116
	Number of triangles      = 5382
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 38734
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 868
	Number of elements       = 4530
	Number of triangles      = 996
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 3534
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 2661
	Number of triangles      = 690
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1971
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 10181
	Number of elements       = 56797
	Number of triangles      = 6782
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 10671
	Number of elements       = 58561
	Number of triangles      = 8546
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 50015
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 7741
	Number of elements       = 43010
	Number of triangles      = 5362
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 37648
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 2692
	Number of elements       = 14435
	Number of triangles      = 2800
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11635
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 238
	Number of elements       = 1116
	Number of triangles      = 384
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 732
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1500
	Number of elements       = 7757
	Number of triangles      = 1986
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1564
	Number of elements       = 7881
	Number of triangles      = 2110
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5771
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1160
	Number of elements       = 6087
	Number of triangles      = 1308
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4779
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 1635
	Number of triangles      = 718
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 917
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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       = 159
	Number of triangles      = 84
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 75
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Tecplot file ....
Finished writing Tecplot file

../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 5077
	Number of elements       = 27808
	Number of triangles      = 4070
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23738
	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          = 5223
	Number of elements       = 28360
	Number of triangles      = 4622
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 23738
	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          = 4887
	Number of elements       = 26853
	Number of triangles      = 4038
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 22815
	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          = 336
	Number of elements       = 1507
	Number of triangles      = 584
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 923
	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          = 33090
	Number of elements       = 191624
	Number of triangles      = 8496
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183128
	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          = 36430
	Number of elements       = 204952
	Number of triangles      = 21824
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 183128
	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          = 28936
	Number of elements       = 164394
	Number of triangles      = 15160
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 149234
	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          = 1415
	Number of elements       = 7515
	Number of triangles      = 1456
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6059
	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          = 4115
	Number of elements       = 22780
	Number of triangles      = 2940
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 19840
	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          = 711
	Number of elements       = 3685
	Number of triangles      = 844
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2841
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1253
	Number of elements       = 6578
	Number of triangles      = 1424
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5154
	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          = 16800
	Number of elements       = 95304
	Number of triangles      = 8802
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86502
	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          = 18724
	Number of elements       = 102680
	Number of triangles      = 16178
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 86502
	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          = 12168
	Number of elements       = 68392
	Number of triangles      = 7142
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 61250
	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          = 6556
	Number of elements       = 34288
	Number of triangles      = 9036
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 25252
	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          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	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          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	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          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	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          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	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          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	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          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	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          = 2940
	Number of elements       = 12771
	Number of triangles      = 5452
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7319
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 7319
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 5440
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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          = 2497
	Number of elements       = 10947
	Number of triangles      = 4552
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 6395
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 6395
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 4540
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file

ok
test_setInput (test_aflr3.TestAFLR3.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr3.TestAFLR3.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 5047
	Number of elements       = 27987
	Number of triangles      = 3464
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 24523
	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          = 6442
	Number of elements       = 36024
	Number of triangles      = 4052
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 31972
	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          = 59849
	Number of elements       = 349298
	Number of triangles      = 12928
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 336370
	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          = 59428
	Number of elements       = 346223
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 333795
	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          = 59849
	Number of elements       = 348798
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 336370
	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:62408)
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:62408)
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:62408)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
 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:62408)
 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:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 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:62408)
 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:62408)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
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 STL file ....
Finished writing Binary STL 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 73440
	Sideset: 'Farfield', set_id 1, num_entries 1332
	Sideset: 'Wing1', set_id 2, num_entries 73440
Finished writing Exodus 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 ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file


Writing Binary STL file ....
Finished writing Binary STL 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 vtk file ....

Writing vtk surface file ....

capsGroups found:
  1: Farfield
  2: Wing1
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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 STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'box_tri', blk_id 1, num_entries 9126
	Block: 'cut_tri', blk_id 2, num_entries 1286
	Sideset: 'box', set_id 1, num_entries 9126
	Sideset: 'cut', set_id 2, num_entries 1286
Finished writing Exodus 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 ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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 STL file ....
Finished writing Binary STL 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 16902
	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 16902
	Sideset: 'Spar1', set_id 4, num_entries 422
	Sideset: 'Spar2', set_id 5, num_entries 166
	Sideset: 'Skin_Top', set_id 6, num_entries 8551
Finished writing Exodus 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 ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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) ... skipped 'No astros.exe executable'
test_Plate (test_astros.TestAstros.test_Plate) ... skipped 'No astros.exe executable'
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
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
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
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_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
   (21:29:56) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:30:09) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:30:18) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:30:33) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:30:36) Linearizing cut-cells
   (21:30:36) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:30:36) Computing gradients
   (21:30:44) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:30:54) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:31:03) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:31:10) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:31:20) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:31:27) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:31:42) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:31:45) Linearizing cut-cells
   (21:31:45) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:31:45) Computing gradients
   (21:31:53) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:32:02) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:32:12) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:32:19) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:32:29) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:32:36) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:32:47) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:32:50) Linearizing cut-cells
   (21:32:50) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:32:50) Computing gradients
   (21:32:54) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:33:03) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:33:13) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:33:20) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:33:30) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:33:37) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:33:49) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:33:52) Linearizing cut-cells
   (21:33:52) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:33:52) Computing gradients
   (21:33:56) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:34:04) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:34:14) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:34:21) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:34:31) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:34:38) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:34:50) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:34:53) Linearizing cut-cells
   (21:34:53) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:34:53) Computing gradients
   (21:34:57) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:35:05) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:35:16) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:35:22) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:35:32) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:35:39) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:35:51) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:35:54) Linearizing cut-cells
   (21:35:54) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:35:54) Computing gradients
   (21:35:58) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:36:07) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:36:17) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:36:24) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:36:34) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:36:41) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:36:53) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:36:56) Linearizing cut-cells
   (21:36:56) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:36:56) Computing gradients
   (21:37:00) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:37:08) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:37:18) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:37:25) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:37:35) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:37:42) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:37:54) 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:        4
              # DVs:                    1
   o Number of simultaneous cutter jobs:   1
   (21:37:57) Linearizing cut-cells
   (21:37:57) ... done
   o Number of simultaneous xsensit jobs:  1
   (21:37:57) Computing gradients
   (21:38:01) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:38:09) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:38:20) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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
   (21:38:27) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:38:37) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:38:45) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:39:00) 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:        4
              # DVs:                    2
   o Number of simultaneous cutter jobs:   2
   (21:39:03) Linearizing cut-cells
   (21:39:05) ... done
   o Number of simultaneous xsensit jobs:  2
   (21:39:05) Computing gradients
              Adjusted OMP_NUM_THREADS to 2 for xsensit
   (21:39:13) ... done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
 o Evaluating Cart3D functionals and/or gradients
   ATTENTION: using static geometry ../inputs/Components.i.tri
   (21:39:22) Running aero.csh on 4 core(s) in M0.5A1B0_DP1
   (21:39:32) aero.csh done
 o case M0.5A1B0_DP1, averaging data over 1 cycle(s)
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 38.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 38.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 39.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 39.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 40.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 40.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 41.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 41.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 42.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 42.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 43.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 43.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 44.
Use of uninitialized value in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 44.
Use of uninitialized value $_[1] in printf at /usr/lib/x86_64-linux-gnu/perl-base/IO/Handle.pm line 163, <GEN1> line 44.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 45.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 45.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 45.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 45.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 45.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 45.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 46.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 46.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 46.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 46.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 46.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 46.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 47.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 47.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 47.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 47.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 47.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 47.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 48.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 48.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 48.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 48.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 48.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 48.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 49.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 49.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 49.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 49.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 49.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 49.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 50.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 50.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 50.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 50.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 50.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 50.
Argument "Rolling" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 59.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 59.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 59.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 59.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 59.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 59.
Argument "Pitching" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 60.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 60.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 60.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 60.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 60.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 60.
Argument "Yawing" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 61.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 61.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 61.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 61.
Argument "0)" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 61.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 61.
Argument "X" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 62.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 62.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 62.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 62.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 62.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 62.
Argument "Y" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 63.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 63.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 63.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 63.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 63.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 63.
Argument "Z" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 149, <GEN1> line 64.
Argument "Moment" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 150, <GEN1> line 64.
Argument "Aero" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 151, <GEN1> line 64.
Argument "about" isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 154, <GEN1> line 64.
Argument "0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 155, <GEN1> line 64.
Argument "(0," isn't numeric in multiplication (*) at /home/jenkins/util/cart3d/cart3d_v1.5.9_X86_64_ICC--22.11.16/bin/model2aero.pl line 156, <GEN1> line 64.
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:62408)
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
 7F6BD7FFF640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F6C6F089000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F6C6F089000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
 7F6BD7FFF640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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
 7F6BD77FE640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F6BD77FE640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F6C6F089000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F6C6F089000 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
 7F6C6F089000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F6C6F089000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F6BD77FE640 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F6BD77FE640 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
 7F6C6F089000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F6C6F089000 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 7F6C0CFF9640 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F6C0CFF9640 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:62408)
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:62408)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
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:62408)
 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:62408)
 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:62408)
 CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
 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:62408)
 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:62408)
 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:62408)
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:62408)
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:62408)
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 STL file ....
Finished writing Binary STL 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 19196
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19196
Finished writing Exodus 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 ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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 STL file ....
Finished writing Binary STL 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 14240
	Sideset: 'Farfield', set_id 1, num_entries 12
	Sideset: 'Wing1', set_id 2, num_entries 14240
Finished writing Exodus 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 ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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    = 7766
Number of elements = 15528
Number of triangle elements      = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5870
Number of elements = 11736
Number of triangle elements      = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14124
Total number of elements = 28236
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.124677
Creating surface mesh ...
Surface mesh seconds:  0.026046
Recovering boundaries...
Boundary recovery seconds:  0.089059
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.043007
Recovering Delaunayness...
Delaunay recovery seconds:  0.053967
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  1.93241
Smoothing vertices...
Mesh smoothing seconds:  1.52528
Improving mesh...
Mesh improvement seconds:  0.044446

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.010934
Total running seconds:  3.85034

Statistics:

  Input points: 14124
  Input facets: 28236
  Input segments: 42354
  Input holes: 2
  Input regions: 0

  Mesh points: 33059
  Mesh tetrahedra: 159851
  Mesh faces: 333820
  Mesh faces on exterior boundary: 28236
  Mesh faces on input facets: 28236
  Mesh edges on input segments: 42354
  Steiner points inside domain: 18935

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    = 7766
Number of elements = 15528
Number of triangle elements      = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 5870
Number of elements = 11736
Number of triangle elements      = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 14124
Total number of elements = 28236
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.123533
Creating surface mesh ...
Surface mesh seconds:  0.026104
Recovering boundaries...
Boundary recovery seconds:  0.095661
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.043578
Recovering Delaunayness...
Delaunay recovery seconds:  0.053786
Refining mesh...
  18827 insertions, added 13420 points, 721721 tetrahedra in queue.
  6269 insertions, added 2485 points, 625204 tetrahedra in queue.
  8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds:  1.99736
Smoothing vertices...
Mesh smoothing seconds:  1.63592
Improving mesh...
Mesh improvement seconds:  0.044052

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.010942
Total running seconds:  4.03144

Statistics:

  Input points: 14124
  Input facets: 28236
  Input segments: 42354
  Input holes: 2
  Input regions: 0

  Mesh points: 33059
  Mesh tetrahedra: 159851
  Mesh faces: 333820
  Mesh faces on exterior boundary: 28236
  Mesh faces on input facets: 28236
  Mesh edges on input segments: 42354
  Steiner points inside domain: 18935

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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/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)
	/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/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 /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/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 - 5043, elements - 10074
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 - 5043, elements - 10074
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 - 14124, elements - 28236
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Python library was linked, but will not be used!

Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1692
	Number of elements = 3380
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 3380
	Elemental Quad4 = 0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - box2
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2402
	Number of elements = 2400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Design_Variable_Relation name - thick_box2
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4009
	Number of elements = 8014
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 8014
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6178
	Combined Number of elements = 12347
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12346
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
 CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 4332
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 4332
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 4000
	Number of elements = 7996
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 7996
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 2
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 6169
	Combined Number of elements = 12329
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 12328
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 3
	Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - point
	Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 7
	Design_Variable name - H
	Design_Variable name - L
	Design_Variable name - W
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> L
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 441
	Number of elements = 400
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 400
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 442
	Combined Number of elements = 401
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 0
	Combined Elemental Quad4 = 400
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> x1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m0
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
===> m1
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
Updating mesh element types based on properties input

Getting FEA design variables.......
	Number of design variables          - 4
	Design_Variable name - m0
	Design_Variable name - m1
	Design_Variable name - x0
	Design_Variable name - x1
	Design_Variable_Relation name - mass_point
	Design_Variable_Relation name - rho_madeupium
	Name madeupium not found in attribute map!!!!
	Design_Variable_Relation name - rho_unobtainium
	Name unobtainium not found in attribute map!!!!
	Design_Variable_Relation name - thick_box1
	Number of design variable relations - 4
	Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ... 
Getting CFD design variables.......
	Number of design variables - 4
	Design Variable name - alowervar
	Design Variable name - auppervar
	Design Variable name - classvar
	Design Variable name - ztailvar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - avar
	Done getting CFD design variables
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
 CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ... 
Getting CFD design variables.......
	Number of design variables - 2
	Design Variable name - camber
	Design Variable name - thick
	Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ... 
Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
 CAPS Info: Hit last success -- going live!

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - thick
	Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 4
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wake, index = 3
	Name = Farfield, index = 4
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest1/Scratch/MultiBody/caps.egads'....


Running pointwise......
Pointwise could not obtain a license:

ERROR (LMF-02004): License call failed for feature fidelity_pointwise, version 23.100 and quantity 1. The license server search path is defined as 5280@acdl.mit.edu. The FLEXnet error message is as follows,
    FLEXnet ERROR(-4, 0, 0): Licensed number of users already reached.

Run 'lic_error LMF-02004' for more information.

Please check your license file, network, and license server status.
Failed to execute! (caps_system): cd '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest1/Scratch/MultiBody' && pointwise -b /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Pointwise could not obtain a license:

ERROR (LMF-02004): License call failed for feature fidelity_pointwise, version 23.100 and quantity 1. The license server search path is defined as 5280@acdl.mit.edu. The FLEXnet error message is as follows,
    FLEXnet ERROR(-4, 0, 0): Licensed number of users already reached.

Run 'lic_error LMF-02004' for more information.

Please check your license file, network, and license server status.
Failed to execute! (caps_system): cd '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest1/Scratch/MultiBody' && pointwise -b /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/pointwise/glyph/GeomToMesh.glf caps.egads capsUserDefaults.glf
Number of command line arguments = 2
Tue Jun 18 2024  9:42:49PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 10
    MaxDim                   = 12
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 19 entries.
  Quilt quilt-1: edge tolerance = 5e-07
  Quilt quilt-2: edge tolerance = 6.19964e-05
  Quilt quilt-3: edge tolerance = 6.19964e-05
  Quilt quilt-4: edge tolerance = 6.19964e-05
  Quilt quilt-5: edge tolerance = 6.19964e-05
  Quilt quilt-6: edge tolerance = 6.19964e-05
  Quilt quilt-7: edge tolerance = 6.19964e-05
  Quilt quilt-8: edge tolerance = 6.19964e-05
  Quilt quilt-9: edge tolerance = 6.19964e-05
  Quilt quilt-10: edge tolerance = 8.32899e-05
  Quilt quilt-11: edge tolerance = 8.32899e-05
  Quilt quilt-12: edge tolerance = 8.32899e-05
  Quilt quilt-13: edge tolerance = 8.32899e-05
  Quilt quilt-14: edge tolerance = 8.32899e-05
  Quilt quilt-15: edge tolerance = 8.32899e-05
  Quilt quilt-16: edge tolerance = 8.32899e-05
  Quilt quilt-17: edge tolerance = 8.32899e-05
  Quilt quilt-18: edge tolerance = 6.19601e-06
  Quilt quilt-19: edge tolerance = 6.19601e-06
  Maximum DB edge tolerance = 8.32899e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.665798e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 19 entries.
Quilt list has 19 entries.
Original connector list has 36 entries.
Minimum connector length = 0.00316783
Tolerance = 8.32899e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 36 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 8.329e-05 on con-29
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/36, name = con-1
Checking dimension for connector 2/36, name = con-2
  Changing dimension for connector 2/36 from 10 to 3
Checking dimension for connector 3/36, name = con-3
Checking dimension for connector 4/36, name = con-4
  Changing dimension for connector 4/36 from 10 to 3
Checking dimension for connector 5/36, name = con-5
  Changing dimension for connector 5/36 from 10 to 4
Checking dimension for connector 6/36, name = con-6
Checking dimension for connector 7/36, name = con-7
  Changing dimension for connector 7/36 from 10 to 3
Checking dimension for connector 8/36, name = con-8
Checking dimension for connector 9/36, name = con-9
  Changing dimension for connector 9/36 from 10 to 3
Checking dimension for connector 10/36, name = con-10
  Changing dimension for connector 10/36 from 10 to 3
Checking dimension for connector 11/36, name = con-11
  Changing dimension for connector 11/36 from 10 to 3
Checking dimension for connector 12/36, name = con-12
Checking dimension for connector 13/36, name = con-13
  Changing dimension for connector 13/36 from 10 to 4
Checking dimension for connector 14/36, name = con-14
Checking dimension for connector 15/36, name = con-16
  Changing dimension for connector 15/36 from 10 to 3
Checking dimension for connector 16/36, name = con-17
Checking dimension for connector 17/36, name = con-20
  Changing dimension for connector 17/36 from 10 to 3
Checking dimension for connector 18/36, name = con-21
Checking dimension for connector 19/36, name = con-24
  Changing dimension for connector 19/36 from 10 to 3
Checking dimension for connector 20/36, name = con-25
  Changing dimension for connector 20/36 from 10 to 4
Checking dimension for connector 21/36, name = con-26
Checking dimension for connector 22/36, name = con-27
  Changing dimension for connector 22/36 from 10 to 3
Checking dimension for connector 23/36, name = con-28
Checking dimension for connector 24/36, name = con-29
  Changing dimension for connector 24/36 from 10 to 3
Checking dimension for connector 25/36, name = con-30
  Changing dimension for connector 25/36 from 10 to 3
Checking dimension for connector 26/36, name = con-31
  Changing dimension for connector 26/36 from 10 to 3
Checking dimension for connector 27/36, name = con-32
Checking dimension for connector 28/36, name = con-33
  Changing dimension for connector 28/36 from 10 to 4
Checking dimension for connector 29/36, name = con-34
Checking dimension for connector 30/36, name = con-36
  Changing dimension for connector 30/36 from 10 to 3
Checking dimension for connector 31/36, name = con-37
Checking dimension for connector 32/36, name = con-40
  Changing dimension for connector 32/36 from 10 to 3
Checking dimension for connector 33/36, name = con-41
Checking dimension for connector 34/36, name = con-44
  Changing dimension for connector 34/36 from 10 to 3
Checking dimension for connector 35/36, name = con-45
Checking dimension for connector 36/36, name = con-46
Processing spacing values for connector 1/36, name = con-1
Processing spacing values for connector 2/36, name = con-2
Processing spacing values for connector 3/36, name = con-3
Processing spacing values for connector 4/36, name = con-4
Processing spacing values for connector 5/36, name = con-5
Processing spacing values for connector 6/36, name = con-6
Processing spacing values for connector 7/36, name = con-7
Processing spacing values for connector 8/36, name = con-8
Processing spacing values for connector 9/36, name = con-9
Processing spacing values for connector 10/36, name = con-10
Processing spacing values for connector 11/36, name = con-11
Processing spacing values for connector 12/36, name = con-12
Processing spacing values for connector 13/36, name = con-13
Processing spacing values for connector 14/36, name = con-14
Processing spacing values for connector 15/36, name = con-16
Processing spacing values for connector 16/36, name = con-17
Processing spacing values for connector 17/36, name = con-20
Processing spacing values for connector 18/36, name = con-21
Processing spacing values for connector 19/36, name = con-24
Processing spacing values for connector 20/36, name = con-25
Processing spacing values for connector 21/36, name = con-26
Processing spacing values for connector 22/36, name = con-27
Processing spacing values for connector 23/36, name = con-28
Processing spacing values for connector 24/36, name = con-29
Processing spacing values for connector 25/36, name = con-30
Processing spacing values for connector 26/36, name = con-31
Processing spacing values for connector 27/36, name = con-32
Processing spacing values for connector 28/36, name = con-33
Processing spacing values for connector 29/36, name = con-34
Processing spacing values for connector 30/36, name = con-36
Processing spacing values for connector 31/36, name = con-37
Processing spacing values for connector 32/36, name = con-40
Processing spacing values for connector 33/36, name = con-41
Processing spacing values for connector 34/36, name = con-44
Processing spacing values for connector 35/36, name = con-45
Processing spacing values for connector 36/36, name = con-46
Number of unique endpoints = 24
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/36, con-1.
    Connector dimension changed from 10 to 12, avg. spacing changed from 1.57135 to 1.28565
  Proximity test for connector 2/36, con-2.
    Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625
  Proximity test for connector 3/36, con-3.
    Connector dimension changed from 10 to 12, avg. spacing changed from 1.57135 to 1.28565
  Proximity test for connector 4/36, con-4.
    Connector dimension changed from 3 to 9, avg. spacing changed from 2.5 to 0.625
  Proximity test for connector 5/36, con-5.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.33869 to 0.365097
  Proximity test for connector 6/36, con-6.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 7/36, con-7.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985229 to 0.179133
  Proximity test for connector 8/36, con-8.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
  Proximity test for connector 9/36, con-9.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 10/36, con-10.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 11/36, con-11.
  Proximity test for connector 12/36, con-12.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
  Proximity test for connector 13/36, con-13.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.26705 to 0.34556
  Proximity test for connector 14/36, con-14.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 15/36, con-16.
  Proximity test for connector 16/36, con-17.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 17/36, con-20.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985229 to 0.179133
  Proximity test for connector 18/36, con-21.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 19/36, con-24.
  Proximity test for connector 20/36, con-25.
    Connector dimension changed from 4 to 12, avg. spacing changed from 0.535476 to 0.146039
  Proximity test for connector 21/36, con-26.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.328651 to 0.268896
  Proximity test for connector 22/36, con-27.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.394092 to 0.071653
  Proximity test for connector 23/36, con-28.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.362929 to 0.296942
  Proximity test for connector 24/36, con-29.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.394096 to 0.0716538
  Proximity test for connector 25/36, con-30.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.394096 to 0.0716538
  Proximity test for connector 26/36, con-31.
  Proximity test for connector 27/36, con-32.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.362929 to 0.296942
  Proximity test for connector 28/36, con-33.
    Connector dimension changed from 4 to 12, avg. spacing changed from 0.506821 to 0.138224
  Proximity test for connector 29/36, con-34.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.328652 to 0.268897
  Proximity test for connector 30/36, con-36.
  Proximity test for connector 31/36, con-37.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.328651 to 0.268896
  Proximity test for connector 32/36, con-40.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.394092 to 0.071653
  Proximity test for connector 33/36, con-41.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.328652 to 0.268897
  Proximity test for connector 34/36, con-44.
  Proximity test for connector 35/36, con-45.
    Connector dimension changed from 10 to 12, avg. spacing changed from 27.9253 to 22.8479
  Proximity test for connector 36/36, con-46.
    Connector dimension changed from 10 to 12, avg. spacing changed from 27.9253 to 22.8479
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 12
Connector con-2 current dim = 9
Connector con-3 current dim = 12
Connector con-4 current dim = 9
Connector con-5 current dim = 12
Connector con-6 current dim = 12
Connector con-7 current dim = 12
Connector con-8 current dim = 12
Connector con-9 current dim = 12
Connector con-10 current dim = 12
Connector con-11 current dim = 3
Connector con-12 current dim = 12
Connector con-13 current dim = 12
Connector con-14 current dim = 12
Connector con-16 current dim = 3
Connector con-17 current dim = 12
Connector con-20 current dim = 12
Connector con-21 current dim = 12
Connector con-24 current dim = 3
Connector con-25 current dim = 12
Connector con-26 current dim = 12
Connector con-27 current dim = 12
Connector con-28 current dim = 12
Connector con-29 current dim = 12
Connector con-30 current dim = 12
Connector con-31 current dim = 3
Connector con-32 current dim = 12
Connector con-33 current dim = 12
Connector con-34 current dim = 12
Connector con-36 current dim = 3
Connector con-37 current dim = 12
Connector con-40 current dim = 12
Connector con-41 current dim = 12
Connector con-44 current dim = 3
Connector con-45 current dim = 12
Connector con-46 current dim = 12
Domain list has 19 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 8.32899e-05
Number of periodic target domains = 0
Unstructured domain 1 of 19:
  boundary name = Wake.
Unstructured domain 2 of 19:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 3 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 4 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 5 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 6 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 7 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 8 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 19:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 10 of 19:
  boundary name = Wing2.
    Creating boundary name Wing2
Unstructured domain 11 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 12 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 13 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 14 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 15 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 16 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 17 of 19:
  boundary name = Wing2.
    Wing2 already in boundary name list.
Unstructured domain 18 of 19:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 19 of 19:
  boundary name = Farfield.
    Farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Number of baffles = 1
Adjusting connector dimensions and distributions for wake treatment.
Number of exit connectors = 0
Number of wake edge connectors = 4
Number of TE connectors = 0
Number of exit nodes = 0
Number of TE nodes = 0
New minimum spacing for Wake treatment = 1.0e20
  WARNING: T-Rex wall boundary con-1 not found!
  WARNING: T-Rex wall boundary con-2 not found!
  WARNING: T-Rex wall boundary con-3 not found!
  WARNING: T-Rex wall boundary con-4 not found!
Adding Edge connector con-1 to redimension list.
Adding Edge connector con-2 to redimension list.
Adding Edge connector con-3 to redimension list.
Adding Edge connector con-4 to redimension list.
Checking connector con-1
Checking connector con-2
Checking connector con-3
Checking connector con-4
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 19 entries.
Baffle domain quilt-1-dom
Number of baffles = 1
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 18 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
Warning: Potential Iso Tet Boundary Recovery Problems
Warning: Out of 2054 tris, 40 have high aspect ratio.
Warning: Max. Normalized Aspect Ratio of 168: 5.01460861086452 4.12134599471833 -0.211064115939546
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:42:56PM EDT
Run Time: 00 Hours 00 Minutes 07 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:42:56PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 104 / 104 curves to EGADS originals
GMA contains 36 edge groups
GMA contains 19 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:42:58PM EDT
Export Time: 00 Hours 00 Minutes 02 Seconds
Volume mesh:
	Number of nodes          = 15180
	Number of elements       = 89853
	Number of triangles      = 1878
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 89853
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 351
	Number of elements = 698
	Number of tris = 698
	Number of quad = 0
Body = 2
	Number of nodes    = 356
	Number of elements = 708
	Number of tris = 708
	Number of quad = 0
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Body = 3
	Number of nodes    = 108
	Number of elements = 176
	Number of tris = 176
	Number of quad = 0
Body = 4
	Number of nodes    = 238
	Number of elements = 472
	Number of tris = 472
	Number of quad = 0
ok
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... 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 global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest2/Scratch/SingleBody/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:04PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 10
    MaxDim                   = 12
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 14 entries.
  Quilt quilt-1: edge tolerance = 5e-07
  Quilt quilt-2: edge tolerance = 5e-07
  Quilt quilt-3: edge tolerance = 5e-07
  Quilt quilt-4: edge tolerance = 5e-07
  Quilt quilt-5: edge tolerance = 5e-07
  Quilt quilt-6: edge tolerance = 5e-07
  Quilt quilt-7: edge tolerance = 6.19964e-05
  Quilt quilt-8: edge tolerance = 6.19964e-05
  Quilt quilt-9: edge tolerance = 6.19964e-05
  Quilt quilt-10: edge tolerance = 6.19964e-05
  Quilt quilt-11: edge tolerance = 6.19964e-05
  Quilt quilt-12: edge tolerance = 6.19964e-05
  Quilt quilt-13: edge tolerance = 6.19964e-05
  Quilt quilt-14: edge tolerance = 6.19964e-05
  Maximum DB edge tolerance = 6.19964e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.239928e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 14 entries.
Quilt list has 14 entries.
Original connector list has 27 entries.
Minimum connector length = 0.00791958
Tolerance = 6.19964e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 27 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 6.200e-05 on con-20
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/27, name = con-1
Checking dimension for connector 2/27, name = con-2
Checking dimension for connector 3/27, name = con-3
Checking dimension for connector 4/27, name = con-4
Checking dimension for connector 5/27, name = con-5
Checking dimension for connector 6/27, name = con-6
Checking dimension for connector 7/27, name = con-7
Checking dimension for connector 8/27, name = con-8
Checking dimension for connector 9/27, name = con-9
Checking dimension for connector 10/27, name = con-11
Checking dimension for connector 11/27, name = con-13
Checking dimension for connector 12/27, name = con-15
Checking dimension for connector 13/27, name = con-16
  Changing dimension for connector 13/27 from 10 to 3
Checking dimension for connector 14/27, name = con-17
  Changing dimension for connector 14/27 from 10 to 3
Checking dimension for connector 15/27, name = con-18
  Changing dimension for connector 15/27 from 10 to 3
Checking dimension for connector 16/27, name = con-19
  Changing dimension for connector 16/27 from 10 to 3
Checking dimension for connector 17/27, name = con-20
  Changing dimension for connector 17/27 from 10 to 3
Checking dimension for connector 18/27, name = con-21
  Changing dimension for connector 18/27 from 10 to 3
Checking dimension for connector 19/27, name = con-22
Checking dimension for connector 20/27, name = con-23
  Changing dimension for connector 20/27 from 10 to 3
Checking dimension for connector 21/27, name = con-24
Checking dimension for connector 22/27, name = con-26
  Changing dimension for connector 22/27 from 10 to 4
Checking dimension for connector 23/27, name = con-27
Checking dimension for connector 24/27, name = con-29
  Changing dimension for connector 24/27 from 10 to 4
Checking dimension for connector 25/27, name = con-31
Checking dimension for connector 26/27, name = con-33
Checking dimension for connector 27/27, name = con-37
Processing spacing values for connector 1/27, name = con-1
Processing spacing values for connector 2/27, name = con-2
Processing spacing values for connector 3/27, name = con-3
Processing spacing values for connector 4/27, name = con-4
Processing spacing values for connector 5/27, name = con-5
Processing spacing values for connector 6/27, name = con-6
Processing spacing values for connector 7/27, name = con-7
Processing spacing values for connector 8/27, name = con-8
Processing spacing values for connector 9/27, name = con-9
Processing spacing values for connector 10/27, name = con-11
Processing spacing values for connector 11/27, name = con-13
Processing spacing values for connector 12/27, name = con-15
Processing spacing values for connector 13/27, name = con-16
Processing spacing values for connector 14/27, name = con-17
Processing spacing values for connector 15/27, name = con-18
Processing spacing values for connector 16/27, name = con-19
Processing spacing values for connector 17/27, name = con-20
Processing spacing values for connector 18/27, name = con-21
Processing spacing values for connector 19/27, name = con-22
Processing spacing values for connector 20/27, name = con-23
Processing spacing values for connector 21/27, name = con-24
Processing spacing values for connector 22/27, name = con-26
Processing spacing values for connector 23/27, name = con-27
Processing spacing values for connector 24/27, name = con-29
Processing spacing values for connector 25/27, name = con-31
Processing spacing values for connector 26/27, name = con-33
Processing spacing values for connector 27/27, name = con-37
Number of unique endpoints = 17
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/27, con-1.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 2/27, con-2.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 3/27, con-3.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 4/27, con-4.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 5/27, con-5.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 6/27, con-6.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 7/27, con-7.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 8/27, con-8.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 9/27, con-9.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 10/27, con-11.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 11/27, con-13.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 12/27, con-15.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 13/27, con-16.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 14/27, con-17.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 15/27, con-18.
  Proximity test for connector 16/27, con-19.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 17/27, con-20.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 18/27, con-21.
  Proximity test for connector 19/27, con-22.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 20/27, con-23.
  Proximity test for connector 21/27, con-24.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 22/27, con-26.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.33869 to 0.365097
  Proximity test for connector 23/27, con-27.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
  Proximity test for connector 24/27, con-29.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.26705 to 0.34556
  Proximity test for connector 25/27, con-31.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 26/27, con-33.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 27/27, con-37.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 12
Connector con-2 current dim = 12
Connector con-3 current dim = 12
Connector con-4 current dim = 12
Connector con-5 current dim = 12
Connector con-6 current dim = 12
Connector con-7 current dim = 12
Connector con-8 current dim = 12
Connector con-9 current dim = 12
Connector con-11 current dim = 12
Connector con-13 current dim = 12
Connector con-15 current dim = 12
Connector con-16 current dim = 12
Connector con-17 current dim = 12
Connector con-18 current dim = 3
Connector con-19 current dim = 12
Connector con-20 current dim = 12
Connector con-21 current dim = 3
Connector con-22 current dim = 12
Connector con-23 current dim = 3
Connector con-24 current dim = 12
Connector con-26 current dim = 12
Connector con-27 current dim = 12
Connector con-29 current dim = 12
Connector con-31 current dim = 12
Connector con-33 current dim = 12
Connector con-37 current dim = 12
Domain list has 14 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 6.19964e-05
Number of periodic target domains = 0
Unstructured domain 1 of 14:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 2 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 3 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 4 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 5 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 6 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 7 of 14:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 8 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 10 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 11 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 12 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 13 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 14 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 14 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 14 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
Warning: Potential Iso Tet Boundary Recovery Problems
Warning: Out of 3006 tris, 20 have high aspect ratio.
Warning: Max. Normalized Aspect Ratio of 168: 5.01460861086452 4.12134599471833 -0.211064115939546
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:43:10PM EDT
Run Time: 00 Hours 00 Minutes 06 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:43:10PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 81 / 81 curves to EGADS originals
GMA contains 27 edge groups
GMA contains 14 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:43:12PM EDT
Export Time: 00 Hours 00 Minutes 02 Seconds
Volume mesh:
	Number of nodes          = 9770
	Number of elements       = 55013
	Number of triangles      = 3006
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 55013
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 1507
	Number of elements = 3006
	Number of tris = 3006
	Number of quad = 0
ok
test_all (test_pointwise.TestPointwise.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62408)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = box, index = 1
	Name = cone, index = 2
	Name = sphere, index = 3
	Name = bullet, index = 4
	Name = farfield, index = 5
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/All/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:17PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 20 entries.
  Quilt quilt-1: edge tolerance = 5e-08
  Quilt quilt-2: edge tolerance = 5e-08
  Quilt quilt-3: edge tolerance = 5e-08
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 2.76557e-06
  Quilt quilt-8: edge tolerance = 2.76557e-06
  Quilt quilt-9: edge tolerance = 2.76557e-06
  Quilt quilt-10: edge tolerance = 6.91474e-06
  Quilt quilt-11: edge tolerance = 6.91474e-06
  Quilt quilt-12: edge tolerance = 5e-08
  Quilt quilt-13: edge tolerance = 2.40433e-07
  Quilt quilt-14: edge tolerance = 2.40433e-07
  Quilt quilt-15: edge tolerance = 5e-08
  Quilt quilt-16: edge tolerance = 5e-08
  Quilt quilt-17: edge tolerance = 5e-08
  Quilt quilt-18: edge tolerance = 5e-08
  Quilt quilt-19: edge tolerance = 5e-08
  Quilt quilt-20: edge tolerance = 5e-08
  Maximum DB edge tolerance = 6.91474e-06
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.382948e-05 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 20 entries.
Quilt list has 20 entries.
Original connector list has 34 entries.
Minimum connector length = 0.322396
Tolerance = 6.91474e-06
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 34 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-1
Max Edge Tol: 6.915e-06 on con-21
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/34, name = con-1
Checking dimension for connector 2/34, name = con-2
Checking dimension for connector 3/34, name = con-3
Checking dimension for connector 4/34, name = con-4
Checking dimension for connector 5/34, name = con-5
Checking dimension for connector 6/34, name = con-6
Checking dimension for connector 7/34, name = con-7
Checking dimension for connector 8/34, name = con-8
Checking dimension for connector 9/34, name = con-9
Checking dimension for connector 10/34, name = con-11
Checking dimension for connector 11/34, name = con-13
Checking dimension for connector 12/34, name = con-15
Checking dimension for connector 13/34, name = con-16
Checking dimension for connector 14/34, name = con-17
  Changing dimension for connector 14/34 from 6 to 3
Checking dimension for connector 15/34, name = con-18
  Changing dimension for connector 15/34 from 6 to 3
Checking dimension for connector 16/34, name = con-20
Checking dimension for connector 17/34, name = con-21
Checking dimension for connector 18/34, name = con-22
Checking dimension for connector 19/34, name = con-23
  Changing dimension for connector 19/34 from 6 to 3
Checking dimension for connector 20/34, name = con-24
Checking dimension for connector 21/34, name = con-25
Checking dimension for connector 22/34, name = con-27
  Changing dimension for connector 22/34 from 6 to 3
Checking dimension for connector 23/34, name = con-28
  Changing dimension for connector 23/34 from 6 to 3
Checking dimension for connector 24/34, name = con-29
  Changing dimension for connector 24/34 from 6 to 3
Checking dimension for connector 25/34, name = con-30
  Changing dimension for connector 25/34 from 6 to 3
Checking dimension for connector 26/34, name = con-31
  Changing dimension for connector 26/34 from 6 to 3
Checking dimension for connector 27/34, name = con-32
  Changing dimension for connector 27/34 from 6 to 3
Checking dimension for connector 28/34, name = con-33
  Changing dimension for connector 28/34 from 6 to 3
Checking dimension for connector 29/34, name = con-34
  Changing dimension for connector 29/34 from 6 to 3
Checking dimension for connector 30/34, name = con-35
  Changing dimension for connector 30/34 from 6 to 3
Checking dimension for connector 31/34, name = con-36
Checking dimension for connector 32/34, name = con-38
Checking dimension for connector 33/34, name = con-40
Checking dimension for connector 34/34, name = con-42
Processing spacing values for connector 1/34, name = con-1
Processing spacing values for connector 2/34, name = con-2
Processing spacing values for connector 3/34, name = con-3
Processing spacing values for connector 4/34, name = con-4
Processing spacing values for connector 5/34, name = con-5
Processing spacing values for connector 6/34, name = con-6
Processing spacing values for connector 7/34, name = con-7
Processing spacing values for connector 8/34, name = con-8
Processing spacing values for connector 9/34, name = con-9
Processing spacing values for connector 10/34, name = con-11
Processing spacing values for connector 11/34, name = con-13
Processing spacing values for connector 12/34, name = con-15
Processing spacing values for connector 13/34, name = con-16
Processing spacing values for connector 14/34, name = con-17
Processing spacing values for connector 15/34, name = con-18
Processing spacing values for connector 16/34, name = con-20
Processing spacing values for connector 17/34, name = con-21
Processing spacing values for connector 18/34, name = con-22
Processing spacing values for connector 19/34, name = con-23
Processing spacing values for connector 20/34, name = con-24
Processing spacing values for connector 21/34, name = con-25
Processing spacing values for connector 22/34, name = con-27
Processing spacing values for connector 23/34, name = con-28
Processing spacing values for connector 24/34, name = con-29
Processing spacing values for connector 25/34, name = con-30
Processing spacing values for connector 26/34, name = con-31
Processing spacing values for connector 27/34, name = con-32
Processing spacing values for connector 28/34, name = con-33
Processing spacing values for connector 29/34, name = con-34
Processing spacing values for connector 30/34, name = con-35
Processing spacing values for connector 31/34, name = con-36
Processing spacing values for connector 32/34, name = con-38
Processing spacing values for connector 33/34, name = con-40
Processing spacing values for connector 34/34, name = con-42
Number of unique endpoints = 24
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/34, con-1.
  Proximity test for connector 2/34, con-2.
  Proximity test for connector 3/34, con-3.
  Proximity test for connector 4/34, con-4.
  Proximity test for connector 5/34, con-5.
  Proximity test for connector 6/34, con-6.
  Proximity test for connector 7/34, con-7.
  Proximity test for connector 8/34, con-8.
  Proximity test for connector 9/34, con-9.
  Proximity test for connector 10/34, con-11.
  Proximity test for connector 11/34, con-13.
  Proximity test for connector 12/34, con-15.
  Proximity test for connector 13/34, con-16.
  Proximity test for connector 14/34, con-17.
    Connector dimension changed from 3 to 5, avg. spacing changed from 0.559017 to 0.279508
  Proximity test for connector 15/34, con-18.
    Connector dimension changed from 3 to 5, avg. spacing changed from 0.559017 to 0.279508
  Proximity test for connector 16/34, con-20.
    Connector dimension changed from 6 to 6, avg. spacing changed from 0.314159 to 0.314159
  Proximity test for connector 17/34, con-21.
  Proximity test for connector 18/34, con-22.
  Proximity test for connector 19/34, con-23.
  Proximity test for connector 20/34, con-24.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.301819 to 0.215585
  Proximity test for connector 21/34, con-25.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
  Proximity test for connector 22/34, con-27.
    Connector dimension changed from 3 to 7, avg. spacing changed from 0.589734 to 0.196578
  Proximity test for connector 23/34, con-28.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 24/34, con-29.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 25/34, con-30.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 26/34, con-31.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 27/34, con-32.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 28/34, con-33.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 29/34, con-34.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 30/34, con-35.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 31/34, con-36.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 32/34, con-38.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 33/34, con-40.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 34/34, con-42.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
con-2 Input connector dimension is a double = 2.00000000000000e+00 
Rounding to integer = 2
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 6
Connector con-2 current dim = 6
Connector con-3 current dim = 6
Connector con-4 current dim = 6
Connector con-5 current dim = 6
Connector con-6 current dim = 6
Connector con-7 current dim = 6
Connector con-8 current dim = 6
Connector con-9 current dim = 6
Connector con-11 current dim = 6
Connector con-13 current dim = 6
Connector con-15 current dim = 6
Connector con-16 current dim = 6
Connector con-17 current dim = 5
Connector con-18 current dim = 5
Connector con-20 current dim = 6
Connector con-21 current dim = 6
Connector con-22 current dim = 6
Connector con-23 current dim = 3
Connector con-24 current dim = 8
Connector con-25 current dim = 8
Connector con-27 current dim = 7
Connector con-28 current dim = 8
Connector con-29 current dim = 8
Connector con-30 current dim = 8
Connector con-31 current dim = 8
Connector con-32 current dim = 8
Connector con-33 current dim = 7
Connector con-34 current dim = 7
Connector con-35 current dim = 7
Connector con-36 current dim = 8
Connector con-38 current dim = 8
Connector con-40 current dim = 8
Connector con-42 current dim = 8
Domain list has 20 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 6.91474e-06
Number of periodic target domains = 0
Unstructured domain 1 of 20:
  boundary name = box.
    Creating boundary name box
Unstructured domain 2 of 20:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 3 of 20:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 4 of 20:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 5 of 20:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 6 of 20:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 7 of 20:
  boundary name = cone.
    Creating boundary name cone
Unstructured domain 8 of 20:
  boundary name = cone.
    cone already in boundary name list.
Unstructured domain 9 of 20:
  boundary name = cone.
    cone already in boundary name list.
Unstructured domain 10 of 20:
  boundary name = sphere.
    Creating boundary name sphere
Unstructured domain 11 of 20:
  boundary name = sphere.
    sphere already in boundary name list.
Unstructured domain 12 of 20:
  boundary name = bullet.
    Creating boundary name bullet
Unstructured domain 13 of 20:
  boundary name = bullet.
    bullet already in boundary name list.
Unstructured domain 14 of 20:
  boundary name = bullet.
    bullet already in boundary name list.
Unstructured domain 15 of 20:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 16 of 20:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 17 of 20:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 18 of 20:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 19 of 20:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 20 of 20:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 20 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 20 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:43:22PM EDT
Run Time: 00 Hours 00 Minutes 05 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:43:22PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 102 / 102 curves to EGADS originals
GMA contains 34 edge groups
GMA contains 20 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:43:24PM EDT
Export Time: 00 Hours 00 Minutes 02 Seconds
Volume mesh:
	Number of nodes          = 2548
	Number of elements       = 13343
	Number of triangles      = 1280
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 13343
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 230
	Number of elements = 456
	Number of tris = 456
	Number of quad = 0
Body = 2
	Number of nodes    = 42
	Number of elements = 80
	Number of tris = 80
	Number of quad = 0
Body = 3
	Number of nodes    = 47
	Number of elements = 90
	Number of tris = 90
	Number of quad = 0
Body = 4
	Number of nodes    = 72
	Number of elements = 140
	Number of tris = 140
	Number of quad = 0
Body = 5
	Number of nodes    = 259
	Number of elements = 514
	Number of tris = 514
	Number of quad = 0
ok
test_box (test_pointwise.TestPointwise.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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Box/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:29PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 12 entries.
  Quilt quilt-1: edge tolerance = 5e-08
  Quilt quilt-2: edge tolerance = 5e-08
  Quilt quilt-3: edge tolerance = 5e-08
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 5e-08
  Quilt quilt-8: edge tolerance = 5e-08
  Quilt quilt-9: edge tolerance = 5e-08
  Quilt quilt-10: edge tolerance = 5e-08
  Quilt quilt-11: edge tolerance = 5e-08
  Quilt quilt-12: edge tolerance = 5e-08
  Maximum DB edge tolerance = 5e-08
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.000000e-07 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 12 entries.
Quilt list has 12 entries.
Original connector list has 24 entries.
Minimum connector length = 1
Tolerance = 5e-08
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 24 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-1
Max Edge Tol: 5.000e-08 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/24, name = con-1
Checking dimension for connector 2/24, name = con-2
Checking dimension for connector 3/24, name = con-3
Checking dimension for connector 4/24, name = con-4
Checking dimension for connector 5/24, name = con-5
Checking dimension for connector 6/24, name = con-6
Checking dimension for connector 7/24, name = con-7
Checking dimension for connector 8/24, name = con-8
Checking dimension for connector 9/24, name = con-9
Checking dimension for connector 10/24, name = con-11
Checking dimension for connector 11/24, name = con-13
Checking dimension for connector 12/24, name = con-15
Checking dimension for connector 13/24, name = con-16
  Changing dimension for connector 13/24 from 6 to 3
Checking dimension for connector 14/24, name = con-17
  Changing dimension for connector 14/24 from 6 to 3
Checking dimension for connector 15/24, name = con-18
  Changing dimension for connector 15/24 from 6 to 3
Checking dimension for connector 16/24, name = con-19
  Changing dimension for connector 16/24 from 6 to 3
Checking dimension for connector 17/24, name = con-20
  Changing dimension for connector 17/24 from 6 to 3
Checking dimension for connector 18/24, name = con-21
  Changing dimension for connector 18/24 from 6 to 3
Checking dimension for connector 19/24, name = con-22
  Changing dimension for connector 19/24 from 6 to 3
Checking dimension for connector 20/24, name = con-23
  Changing dimension for connector 20/24 from 6 to 3
Checking dimension for connector 21/24, name = con-24
Checking dimension for connector 22/24, name = con-26
Checking dimension for connector 23/24, name = con-28
Checking dimension for connector 24/24, name = con-30
Processing spacing values for connector 1/24, name = con-1
Processing spacing values for connector 2/24, name = con-2
Processing spacing values for connector 3/24, name = con-3
Processing spacing values for connector 4/24, name = con-4
Processing spacing values for connector 5/24, name = con-5
Processing spacing values for connector 6/24, name = con-6
Processing spacing values for connector 7/24, name = con-7
Processing spacing values for connector 8/24, name = con-8
Processing spacing values for connector 9/24, name = con-9
Processing spacing values for connector 10/24, name = con-11
Processing spacing values for connector 11/24, name = con-13
Processing spacing values for connector 12/24, name = con-15
Processing spacing values for connector 13/24, name = con-16
Processing spacing values for connector 14/24, name = con-17
Processing spacing values for connector 15/24, name = con-18
Processing spacing values for connector 16/24, name = con-19
Processing spacing values for connector 17/24, name = con-20
Processing spacing values for connector 18/24, name = con-21
Processing spacing values for connector 19/24, name = con-22
Processing spacing values for connector 20/24, name = con-23
Processing spacing values for connector 21/24, name = con-24
Processing spacing values for connector 22/24, name = con-26
Processing spacing values for connector 23/24, name = con-28
Processing spacing values for connector 24/24, name = con-30
Number of unique endpoints = 16
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/24, con-1.
  Proximity test for connector 2/24, con-2.
  Proximity test for connector 3/24, con-3.
  Proximity test for connector 4/24, con-4.
  Proximity test for connector 5/24, con-5.
  Proximity test for connector 6/24, con-6.
  Proximity test for connector 7/24, con-7.
  Proximity test for connector 8/24, con-8.
  Proximity test for connector 9/24, con-9.
  Proximity test for connector 10/24, con-11.
  Proximity test for connector 11/24, con-13.
  Proximity test for connector 12/24, con-15.
  Proximity test for connector 13/24, con-16.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 14/24, con-17.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 15/24, con-18.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 16/24, con-19.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 17/24, con-20.
  Proximity test for connector 18/24, con-21.
  Proximity test for connector 19/24, con-22.
  Proximity test for connector 20/24, con-23.
  Proximity test for connector 21/24, con-24.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 22/24, con-26.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 23/24, con-28.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 24/24, con-30.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
con-2 Input connector dimension is a double = 2.00000000000000e+00 
Rounding to integer = 2
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 6
Connector con-2 current dim = 6
Connector con-3 current dim = 6
Connector con-4 current dim = 6
Connector con-5 current dim = 6
Connector con-6 current dim = 6
Connector con-7 current dim = 6
Connector con-8 current dim = 6
Connector con-9 current dim = 6
Connector con-11 current dim = 6
Connector con-13 current dim = 6
Connector con-15 current dim = 6
Connector con-16 current dim = 8
Connector con-17 current dim = 8
Connector con-18 current dim = 8
Connector con-19 current dim = 8
Connector con-20 current dim = 3
Connector con-21 current dim = 3
Connector con-22 current dim = 3
Connector con-23 current dim = 3
Connector con-24 current dim = 8
Connector con-26 current dim = 8
Connector con-28 current dim = 8
Connector con-30 current dim = 8
Domain list has 12 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 5e-08
Number of periodic target domains = 0
Unstructured domain 1 of 12:
  boundary name = box.
    Creating boundary name box
Unstructured domain 2 of 12:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 3 of 12:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 4 of 12:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 5 of 12:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 6 of 12:
  boundary name = box.
    box already in boundary name list.
Unstructured domain 7 of 12:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 8 of 12:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 9 of 12:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 10 of 12:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 11 of 12:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 12 of 12:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 12 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 12 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:43:33PM EDT
Run Time: 00 Hours 00 Minutes 04 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:43:33PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 72 / 72 curves to EGADS originals
GMA contains 24 edge groups
GMA contains 12 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:43:34PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
	Number of nodes          = 1190
	Number of elements       = 5908
	Number of triangles      = 824
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 5908
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 230
	Number of elements = 456
	Number of tris = 456
	Number of quad = 0
Body = 2
	Number of nodes    = 186
	Number of elements = 368
	Number of tris = 368
	Number of quad = 0
ok
test_bullet (test_pointwise.TestPointwise.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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Bullet/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:39PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 9 entries.
  Quilt quilt-1: edge tolerance = 5e-08
  Quilt quilt-2: edge tolerance = 2.40433e-07
  Quilt quilt-3: edge tolerance = 2.40433e-07
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 5e-08
  Quilt quilt-8: edge tolerance = 5e-08
  Quilt quilt-9: edge tolerance = 5e-08
  Maximum DB edge tolerance = 2.40433e-07
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 4.808651e-07 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 9 entries.
Quilt list has 9 entries.
Original connector list has 16 entries.
Minimum connector length = 0.322396
Tolerance = 2.40433e-07
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 16 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-6
Max Edge Tol: 2.404e-07 on con-3
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/16, name = con-1
  Changing dimension for connector 1/16 from 6 to 3
Checking dimension for connector 2/16, name = con-2
Checking dimension for connector 3/16, name = con-3
Checking dimension for connector 4/16, name = con-5
  Changing dimension for connector 4/16 from 6 to 3
Checking dimension for connector 5/16, name = con-6
  Changing dimension for connector 5/16 from 6 to 3
Checking dimension for connector 6/16, name = con-7
  Changing dimension for connector 6/16 from 6 to 3
Checking dimension for connector 7/16, name = con-8
  Changing dimension for connector 7/16 from 6 to 3
Checking dimension for connector 8/16, name = con-9
  Changing dimension for connector 8/16 from 6 to 3
Checking dimension for connector 9/16, name = con-10
  Changing dimension for connector 9/16 from 6 to 3
Checking dimension for connector 10/16, name = con-11
  Changing dimension for connector 10/16 from 6 to 3
Checking dimension for connector 11/16, name = con-12
  Changing dimension for connector 11/16 from 6 to 3
Checking dimension for connector 12/16, name = con-13
  Changing dimension for connector 12/16 from 6 to 3
Checking dimension for connector 13/16, name = con-14
Checking dimension for connector 14/16, name = con-16
Checking dimension for connector 15/16, name = con-18
Checking dimension for connector 16/16, name = con-20
Processing spacing values for connector 1/16, name = con-1
Processing spacing values for connector 2/16, name = con-2
Processing spacing values for connector 3/16, name = con-3
Processing spacing values for connector 4/16, name = con-5
Processing spacing values for connector 5/16, name = con-6
Processing spacing values for connector 6/16, name = con-7
Processing spacing values for connector 7/16, name = con-8
Processing spacing values for connector 8/16, name = con-9
Processing spacing values for connector 9/16, name = con-10
Processing spacing values for connector 10/16, name = con-11
Processing spacing values for connector 11/16, name = con-12
Processing spacing values for connector 12/16, name = con-13
Processing spacing values for connector 13/16, name = con-14
Processing spacing values for connector 14/16, name = con-16
Processing spacing values for connector 15/16, name = con-18
Processing spacing values for connector 16/16, name = con-20
Number of unique endpoints = 11
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/16, con-1.
  Proximity test for connector 2/16, con-2.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.301819 to 0.215585
  Proximity test for connector 3/16, con-3.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
  Proximity test for connector 4/16, con-5.
    Connector dimension changed from 3 to 7, avg. spacing changed from 0.589734 to 0.196578
  Proximity test for connector 5/16, con-6.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 6/16, con-7.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 7/16, con-8.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 8/16, con-9.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 9/16, con-10.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2 to 0.571429
  Proximity test for connector 10/16, con-11.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 11/16, con-12.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 12/16, con-13.
    Connector dimension changed from 3 to 7, avg. spacing changed from 2 to 0.666667
  Proximity test for connector 13/16, con-14.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 14/16, con-16.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 15/16, con-18.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 16/16, con-20.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 3
Connector con-2 current dim = 8
Connector con-3 current dim = 8
Connector con-5 current dim = 7
Connector con-6 current dim = 4
Connector con-7 current dim = 4
Connector con-8 current dim = 4
Connector con-9 current dim = 4
Connector con-10 current dim = 8
Connector con-11 current dim = 7
Connector con-12 current dim = 7
Connector con-13 current dim = 7
Connector con-14 current dim = 8
Connector con-16 current dim = 8
Connector con-18 current dim = 8
Connector con-20 current dim = 8
Domain list has 9 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 2.40433e-07
Number of periodic target domains = 0
Unstructured domain 1 of 9:
  boundary name = bullet.
    Creating boundary name bullet
Unstructured domain 2 of 9:
  boundary name = bullet.
    bullet already in boundary name list.
Unstructured domain 3 of 9:
  boundary name = bullet.
    bullet already in boundary name list.
Unstructured domain 4 of 9:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 5 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 6 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 7 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 8 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 9 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 9 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 9 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:43:42PM EDT
Run Time: 00 Hours 00 Minutes 03 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:43:42PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 48 / 48 curves to EGADS originals
GMA contains 16 edge groups
GMA contains 9 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:43:43PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
	Number of nodes          = 876
	Number of elements       = 4439
	Number of triangles      = 488
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4439
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 72
	Number of elements = 140
	Number of tris = 140
	Number of quad = 0
Body = 2
	Number of nodes    = 176
	Number of elements = 348
	Number of tris = 348
	Number of quad = 0
ok
test_cone (test_pointwise.TestPointwise.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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Cone/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:48PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 9 entries.
  Quilt quilt-1: edge tolerance = 2.76557e-06
  Quilt quilt-2: edge tolerance = 2.76557e-06
  Quilt quilt-3: edge tolerance = 2.76557e-06
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 5e-08
  Quilt quilt-8: edge tolerance = 5e-08
  Quilt quilt-9: edge tolerance = 5e-08
  Maximum DB edge tolerance = 2.76557e-06
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 5.531142e-06 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 9 entries.
Quilt list has 9 entries.
Original connector list has 16 entries.
Minimum connector length = 1.11803
Tolerance = 2.76557e-06
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 16 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-6
Max Edge Tol: 2.766e-06 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/16, name = con-1
Checking dimension for connector 2/16, name = con-2
  Changing dimension for connector 2/16 from 6 to 3
Checking dimension for connector 3/16, name = con-3
  Changing dimension for connector 3/16 from 6 to 3
Checking dimension for connector 4/16, name = con-5
Checking dimension for connector 5/16, name = con-6
  Changing dimension for connector 5/16 from 6 to 3
Checking dimension for connector 6/16, name = con-7
  Changing dimension for connector 6/16 from 6 to 3
Checking dimension for connector 7/16, name = con-8
  Changing dimension for connector 7/16 from 6 to 3
Checking dimension for connector 8/16, name = con-9
  Changing dimension for connector 8/16 from 6 to 3
Checking dimension for connector 9/16, name = con-10
  Changing dimension for connector 9/16 from 6 to 3
Checking dimension for connector 10/16, name = con-11
  Changing dimension for connector 10/16 from 6 to 3
Checking dimension for connector 11/16, name = con-12
  Changing dimension for connector 11/16 from 6 to 3
Checking dimension for connector 12/16, name = con-13
  Changing dimension for connector 12/16 from 6 to 3
Checking dimension for connector 13/16, name = con-14
Checking dimension for connector 14/16, name = con-16
Checking dimension for connector 15/16, name = con-18
Checking dimension for connector 16/16, name = con-20
Processing spacing values for connector 1/16, name = con-1
Processing spacing values for connector 2/16, name = con-2
Processing spacing values for connector 3/16, name = con-3
Processing spacing values for connector 4/16, name = con-5
Processing spacing values for connector 5/16, name = con-6
Processing spacing values for connector 6/16, name = con-7
Processing spacing values for connector 7/16, name = con-8
Processing spacing values for connector 8/16, name = con-9
Processing spacing values for connector 9/16, name = con-10
Processing spacing values for connector 10/16, name = con-11
Processing spacing values for connector 11/16, name = con-12
Processing spacing values for connector 12/16, name = con-13
Processing spacing values for connector 13/16, name = con-14
Processing spacing values for connector 14/16, name = con-16
Processing spacing values for connector 15/16, name = con-18
Processing spacing values for connector 16/16, name = con-20
Number of unique endpoints = 11
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/16, con-1.
  Proximity test for connector 2/16, con-2.
    Connector dimension changed from 3 to 5, avg. spacing changed from 0.559017 to 0.279508
  Proximity test for connector 3/16, con-3.
    Connector dimension changed from 3 to 5, avg. spacing changed from 0.559017 to 0.279508
  Proximity test for connector 4/16, con-5.
    Connector dimension changed from 6 to 6, avg. spacing changed from 0.314159 to 0.314159
  Proximity test for connector 5/16, con-6.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 6/16, con-7.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 7/16, con-8.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 8/16, con-9.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 9/16, con-10.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 10/16, con-11.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 11/16, con-12.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 12/16, con-13.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 13/16, con-14.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 14/16, con-16.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 15/16, con-18.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 16/16, con-20.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 6
Connector con-2 current dim = 5
Connector con-3 current dim = 5
Connector con-5 current dim = 6
Connector con-6 current dim = 5
Connector con-7 current dim = 5
Connector con-8 current dim = 5
Connector con-9 current dim = 5
Connector con-10 current dim = 4
Connector con-11 current dim = 4
Connector con-12 current dim = 4
Connector con-13 current dim = 4
Connector con-14 current dim = 8
Connector con-16 current dim = 8
Connector con-18 current dim = 8
Connector con-20 current dim = 8
Domain list has 9 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 2.76557e-06
Number of periodic target domains = 0
Unstructured domain 1 of 9:
  boundary name = cone.
    Creating boundary name cone
Unstructured domain 2 of 9:
  boundary name = cone.
    cone already in boundary name list.
Unstructured domain 3 of 9:
  boundary name = cone.
    cone already in boundary name list.
Unstructured domain 4 of 9:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 5 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 6 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 7 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 8 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 9 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 9 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 9 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:43:52PM EDT
Run Time: 00 Hours 00 Minutes 03 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:43:52PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 48 / 48 curves to EGADS originals
GMA contains 16 edge groups
GMA contains 9 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:43:52PM EDT
Export Time: 00 Hours 00 Minutes 00 Seconds
Volume mesh:
	Number of nodes          = 544
	Number of elements       = 2667
	Number of triangles      = 338
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2667
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 42
	Number of elements = 80
	Number of tris = 80
	Number of quad = 0
Body = 2
	Number of nodes    = 131
	Number of elements = 258
	Number of tris = 258
	Number of quad = 0
ok
test_cylinder (test_pointwise.TestPointwise.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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Cylinder/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:43:58PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 9 entries.
  Quilt quilt-1: edge tolerance = 2.40432e-07
  Quilt quilt-2: edge tolerance = 2.40432e-07
  Quilt quilt-3: edge tolerance = 2.40432e-07
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 5e-08
  Quilt quilt-8: edge tolerance = 5e-08
  Quilt quilt-9: edge tolerance = 5e-08
  Maximum DB edge tolerance = 2.40432e-07
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 4.808648e-07 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 9 entries.
Quilt list has 9 entries.
Original connector list has 15 entries.
Minimum connector length = 1
Tolerance = 2.40432e-07
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 15 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-5
Max Edge Tol: 2.404e-07 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/15, name = con-1
Checking dimension for connector 2/15, name = con-2
Checking dimension for connector 3/15, name = con-4
  Changing dimension for connector 3/15 from 6 to 3
Checking dimension for connector 4/15, name = con-5
  Changing dimension for connector 4/15 from 6 to 3
Checking dimension for connector 5/15, name = con-6
  Changing dimension for connector 5/15 from 6 to 3
Checking dimension for connector 6/15, name = con-7
  Changing dimension for connector 6/15 from 6 to 3
Checking dimension for connector 7/15, name = con-8
  Changing dimension for connector 7/15 from 6 to 3
Checking dimension for connector 8/15, name = con-9
  Changing dimension for connector 8/15 from 6 to 3
Checking dimension for connector 9/15, name = con-10
  Changing dimension for connector 9/15 from 6 to 3
Checking dimension for connector 10/15, name = con-11
  Changing dimension for connector 10/15 from 6 to 3
Checking dimension for connector 11/15, name = con-12
  Changing dimension for connector 11/15 from 6 to 3
Checking dimension for connector 12/15, name = con-13
Checking dimension for connector 13/15, name = con-15
Checking dimension for connector 14/15, name = con-17
Checking dimension for connector 15/15, name = con-19
Processing spacing values for connector 1/15, name = con-1
Processing spacing values for connector 2/15, name = con-2
Processing spacing values for connector 3/15, name = con-4
Processing spacing values for connector 4/15, name = con-5
Processing spacing values for connector 5/15, name = con-6
Processing spacing values for connector 6/15, name = con-7
Processing spacing values for connector 7/15, name = con-8
Processing spacing values for connector 8/15, name = con-9
Processing spacing values for connector 9/15, name = con-10
Processing spacing values for connector 10/15, name = con-11
Processing spacing values for connector 11/15, name = con-12
Processing spacing values for connector 12/15, name = con-13
Processing spacing values for connector 13/15, name = con-15
Processing spacing values for connector 14/15, name = con-17
Processing spacing values for connector 15/15, name = con-19
Number of unique endpoints = 10
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/15, con-1.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
  Proximity test for connector 2/15, con-2.
    Connector dimension changed from 6 to 8, avg. spacing changed from 0.628319 to 0.448799
  Proximity test for connector 3/15, con-4.
  Proximity test for connector 4/15, con-5.
    Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
  Proximity test for connector 5/15, con-6.
    Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
  Proximity test for connector 6/15, con-7.
    Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
  Proximity test for connector 7/15, con-8.
    Connector dimension changed from 3 to 6, avg. spacing changed from 2 to 0.8
  Proximity test for connector 8/15, con-9.
  Proximity test for connector 9/15, con-10.
  Proximity test for connector 10/15, con-11.
  Proximity test for connector 11/15, con-12.
  Proximity test for connector 12/15, con-13.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 13/15, con-15.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 14/15, con-17.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 15/15, con-19.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 8
Connector con-2 current dim = 8
Connector con-4 current dim = 3
Connector con-5 current dim = 6
Connector con-6 current dim = 6
Connector con-7 current dim = 6
Connector con-8 current dim = 6
Connector con-9 current dim = 3
Connector con-10 current dim = 3
Connector con-11 current dim = 3
Connector con-12 current dim = 3
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-17 current dim = 8
Connector con-19 current dim = 8
Domain list has 9 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 2.40432e-07
Number of periodic target domains = 0
Unstructured domain 1 of 9:
  boundary name = cylinder.
    Creating boundary name cylinder
Unstructured domain 2 of 9:
  boundary name = cylinder.
    cylinder already in boundary name list.
Unstructured domain 3 of 9:
  boundary name = cylinder.
    cylinder already in boundary name list.
Unstructured domain 4 of 9:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 5 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 6 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 7 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 8 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 9 of 9:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 9 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 9 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:44:01PM EDT
Run Time: 00 Hours 00 Minutes 03 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:44:01PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 45 / 45 curves to EGADS originals
GMA contains 15 edge groups
GMA contains 9 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:44:02PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
	Number of nodes          = 443
	Number of elements       = 2028
	Number of triangles      = 352
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2028
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 39
	Number of elements = 74
	Number of tris = 74
	Number of quad = 0
Body = 2
	Number of nodes    = 141
	Number of elements = 278
	Number of tris = 278
	Number of quad = 0
ok
test_executeError (test_pointwise.TestPointwise.test_executeError) ... 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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/BoxError/caps.egads'....
ok
test_reenter (test_pointwise.TestPointwise.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 global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:44:07PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 10
    MaxDim                   = 12
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 14 entries.
  Quilt quilt-1: edge tolerance = 5e-07
  Quilt quilt-2: edge tolerance = 5e-07
  Quilt quilt-3: edge tolerance = 5e-07
  Quilt quilt-4: edge tolerance = 5e-07
  Quilt quilt-5: edge tolerance = 5e-07
  Quilt quilt-6: edge tolerance = 5e-07
  Quilt quilt-7: edge tolerance = 6.19964e-05
  Quilt quilt-8: edge tolerance = 6.19964e-05
  Quilt quilt-9: edge tolerance = 6.19964e-05
  Quilt quilt-10: edge tolerance = 6.19964e-05
  Quilt quilt-11: edge tolerance = 6.19964e-05
  Quilt quilt-12: edge tolerance = 6.19964e-05
  Quilt quilt-13: edge tolerance = 6.19964e-05
  Quilt quilt-14: edge tolerance = 6.19964e-05
  Maximum DB edge tolerance = 6.19964e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.239928e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 14 entries.
Quilt list has 14 entries.
Original connector list has 27 entries.
Minimum connector length = 0.00791958
Tolerance = 6.19964e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 27 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 6.200e-05 on con-20
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/27, name = con-1
Checking dimension for connector 2/27, name = con-2
Checking dimension for connector 3/27, name = con-3
Checking dimension for connector 4/27, name = con-4
Checking dimension for connector 5/27, name = con-5
Checking dimension for connector 6/27, name = con-6
Checking dimension for connector 7/27, name = con-7
Checking dimension for connector 8/27, name = con-8
Checking dimension for connector 9/27, name = con-9
Checking dimension for connector 10/27, name = con-11
Checking dimension for connector 11/27, name = con-13
Checking dimension for connector 12/27, name = con-15
Checking dimension for connector 13/27, name = con-16
  Changing dimension for connector 13/27 from 10 to 3
Checking dimension for connector 14/27, name = con-17
  Changing dimension for connector 14/27 from 10 to 3
Checking dimension for connector 15/27, name = con-18
  Changing dimension for connector 15/27 from 10 to 3
Checking dimension for connector 16/27, name = con-19
  Changing dimension for connector 16/27 from 10 to 3
Checking dimension for connector 17/27, name = con-20
  Changing dimension for connector 17/27 from 10 to 3
Checking dimension for connector 18/27, name = con-21
  Changing dimension for connector 18/27 from 10 to 3
Checking dimension for connector 19/27, name = con-22
Checking dimension for connector 20/27, name = con-23
  Changing dimension for connector 20/27 from 10 to 3
Checking dimension for connector 21/27, name = con-24
Checking dimension for connector 22/27, name = con-26
  Changing dimension for connector 22/27 from 10 to 4
Checking dimension for connector 23/27, name = con-27
Checking dimension for connector 24/27, name = con-29
  Changing dimension for connector 24/27 from 10 to 4
Checking dimension for connector 25/27, name = con-31
Checking dimension for connector 26/27, name = con-33
Checking dimension for connector 27/27, name = con-37
Processing spacing values for connector 1/27, name = con-1
Processing spacing values for connector 2/27, name = con-2
Processing spacing values for connector 3/27, name = con-3
Processing spacing values for connector 4/27, name = con-4
Processing spacing values for connector 5/27, name = con-5
Processing spacing values for connector 6/27, name = con-6
Processing spacing values for connector 7/27, name = con-7
Processing spacing values for connector 8/27, name = con-8
Processing spacing values for connector 9/27, name = con-9
Processing spacing values for connector 10/27, name = con-11
Processing spacing values for connector 11/27, name = con-13
Processing spacing values for connector 12/27, name = con-15
Processing spacing values for connector 13/27, name = con-16
Processing spacing values for connector 14/27, name = con-17
Processing spacing values for connector 15/27, name = con-18
Processing spacing values for connector 16/27, name = con-19
Processing spacing values for connector 17/27, name = con-20
Processing spacing values for connector 18/27, name = con-21
Processing spacing values for connector 19/27, name = con-22
Processing spacing values for connector 20/27, name = con-23
Processing spacing values for connector 21/27, name = con-24
Processing spacing values for connector 22/27, name = con-26
Processing spacing values for connector 23/27, name = con-27
Processing spacing values for connector 24/27, name = con-29
Processing spacing values for connector 25/27, name = con-31
Processing spacing values for connector 26/27, name = con-33
Processing spacing values for connector 27/27, name = con-37
Number of unique endpoints = 17
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/27, con-1.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 2/27, con-2.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 3/27, con-3.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 4/27, con-4.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 5/27, con-5.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 6/27, con-6.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 7/27, con-7.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 8/27, con-8.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 9/27, con-9.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 10/27, con-11.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 11/27, con-13.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 12/27, con-15.
    Connector dimension changed from 10 to 12, avg. spacing changed from 8.88889 to 7.27273
  Proximity test for connector 13/27, con-16.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 14/27, con-17.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 15/27, con-18.
  Proximity test for connector 16/27, con-19.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 17/27, con-20.
    Connector dimension changed from 3 to 12, avg. spacing changed from 0.985232 to 0.179133
  Proximity test for connector 18/27, con-21.
  Proximity test for connector 19/27, con-22.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 20/27, con-23.
  Proximity test for connector 21/27, con-24.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 22/27, con-26.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.33869 to 0.365097
  Proximity test for connector 23/27, con-27.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
  Proximity test for connector 24/27, con-29.
    Connector dimension changed from 4 to 12, avg. spacing changed from 1.26705 to 0.34556
  Proximity test for connector 25/27, con-31.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821631 to 0.672244
  Proximity test for connector 26/27, con-33.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.821627 to 0.67224
  Proximity test for connector 27/27, con-37.
    Connector dimension changed from 10 to 12, avg. spacing changed from 0.907322 to 0.742354
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 12
Connector con-2 current dim = 12
Connector con-3 current dim = 12
Connector con-4 current dim = 12
Connector con-5 current dim = 12
Connector con-6 current dim = 12
Connector con-7 current dim = 12
Connector con-8 current dim = 12
Connector con-9 current dim = 12
Connector con-11 current dim = 12
Connector con-13 current dim = 12
Connector con-15 current dim = 12
Connector con-16 current dim = 12
Connector con-17 current dim = 12
Connector con-18 current dim = 3
Connector con-19 current dim = 12
Connector con-20 current dim = 12
Connector con-21 current dim = 3
Connector con-22 current dim = 12
Connector con-23 current dim = 3
Connector con-24 current dim = 12
Connector con-26 current dim = 12
Connector con-27 current dim = 12
Connector con-29 current dim = 12
Connector con-31 current dim = 12
Connector con-33 current dim = 12
Connector con-37 current dim = 12
Domain list has 14 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 6.19964e-05
Number of periodic target domains = 0
Unstructured domain 1 of 14:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 2 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 3 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 4 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 5 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 6 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 7 of 14:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 8 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 10 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 11 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 12 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 13 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 14 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 14 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 14 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
Warning: Potential Iso Tet Boundary Recovery Problems
Warning: Out of 3006 tris, 20 have high aspect ratio.
Warning: Max. Normalized Aspect Ratio of 168: 5.01460861086452 4.12134599471833 -0.211064115939546
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:44:13PM EDT
Run Time: 00 Hours 00 Minutes 06 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:44:13PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 81 / 81 curves to EGADS originals
GMA contains 27 edge groups
GMA contains 14 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:44:16PM EDT
Export Time: 00 Hours 00 Minutes 03 Seconds
Volume mesh:
	Number of nodes          = 9770
	Number of elements       = 55013
	Number of triangles      = 3006
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 55013
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 1507
	Number of elements = 3006
	Number of tris = 3006
	Number of quad = 0

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 55013
	Sideset: 'Farfield', set_id 1, num_entries 2298
	Sideset: 'Wing1', set_id 2, num_entries 708
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK 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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest3/Scratch/SingleBody2/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:44:21PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 100
Computing maximum DB edge tolerance.
  Quilt list has 14 entries.
  Quilt quilt-1: edge tolerance = 5e-07
  Quilt quilt-2: edge tolerance = 5e-07
  Quilt quilt-3: edge tolerance = 5e-07
  Quilt quilt-4: edge tolerance = 5e-07
  Quilt quilt-5: edge tolerance = 5e-07
  Quilt quilt-6: edge tolerance = 5e-07
  Quilt quilt-7: edge tolerance = 6.19964e-05
  Quilt quilt-8: edge tolerance = 6.19964e-05
  Quilt quilt-9: edge tolerance = 6.19964e-05
  Quilt quilt-10: edge tolerance = 6.19964e-05
  Quilt quilt-11: edge tolerance = 6.19964e-05
  Quilt quilt-12: edge tolerance = 6.19964e-05
  Quilt quilt-13: edge tolerance = 6.19964e-05
  Quilt quilt-14: edge tolerance = 6.19964e-05
  Maximum DB edge tolerance = 6.19964e-05
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.239928e-04 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 14 entries.
Quilt list has 14 entries.
Original connector list has 27 entries.
Minimum connector length = 0.00791958
Tolerance = 6.19964e-05
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 27 entries.
Updating conData
Min Edge Tol: 5.000e-07 on con-1
Max Edge Tol: 6.200e-05 on con-20
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/27, name = con-1
Checking dimension for connector 2/27, name = con-2
Checking dimension for connector 3/27, name = con-3
Checking dimension for connector 4/27, name = con-4
Checking dimension for connector 5/27, name = con-5
Checking dimension for connector 6/27, name = con-6
Checking dimension for connector 7/27, name = con-7
Checking dimension for connector 8/27, name = con-8
Checking dimension for connector 9/27, name = con-9
Checking dimension for connector 10/27, name = con-11
Checking dimension for connector 11/27, name = con-13
Checking dimension for connector 12/27, name = con-15
Checking dimension for connector 13/27, name = con-16
  Changing dimension for connector 13/27 from 6 to 3
Checking dimension for connector 14/27, name = con-17
  Changing dimension for connector 14/27 from 6 to 3
Checking dimension for connector 15/27, name = con-18
  Changing dimension for connector 15/27 from 6 to 3
Checking dimension for connector 16/27, name = con-19
  Changing dimension for connector 16/27 from 6 to 3
Checking dimension for connector 17/27, name = con-20
  Changing dimension for connector 17/27 from 6 to 3
Checking dimension for connector 18/27, name = con-21
  Changing dimension for connector 18/27 from 6 to 3
Checking dimension for connector 19/27, name = con-22
Checking dimension for connector 20/27, name = con-23
  Changing dimension for connector 20/27 from 6 to 3
Checking dimension for connector 21/27, name = con-24
Checking dimension for connector 22/27, name = con-26
  Changing dimension for connector 22/27 from 6 to 3
Checking dimension for connector 23/27, name = con-27
Checking dimension for connector 24/27, name = con-29
  Changing dimension for connector 24/27 from 6 to 3
Checking dimension for connector 25/27, name = con-31
Checking dimension for connector 26/27, name = con-33
Checking dimension for connector 27/27, name = con-37
Processing spacing values for connector 1/27, name = con-1
Processing spacing values for connector 2/27, name = con-2
Processing spacing values for connector 3/27, name = con-3
Processing spacing values for connector 4/27, name = con-4
Processing spacing values for connector 5/27, name = con-5
Processing spacing values for connector 6/27, name = con-6
Processing spacing values for connector 7/27, name = con-7
Processing spacing values for connector 8/27, name = con-8
Processing spacing values for connector 9/27, name = con-9
Processing spacing values for connector 10/27, name = con-11
Processing spacing values for connector 11/27, name = con-13
Processing spacing values for connector 12/27, name = con-15
Processing spacing values for connector 13/27, name = con-16
Processing spacing values for connector 14/27, name = con-17
Processing spacing values for connector 15/27, name = con-18
Processing spacing values for connector 16/27, name = con-19
Processing spacing values for connector 17/27, name = con-20
Processing spacing values for connector 18/27, name = con-21
Processing spacing values for connector 19/27, name = con-22
Processing spacing values for connector 20/27, name = con-23
Processing spacing values for connector 21/27, name = con-24
Processing spacing values for connector 22/27, name = con-26
Processing spacing values for connector 23/27, name = con-27
Processing spacing values for connector 24/27, name = con-29
Processing spacing values for connector 25/27, name = con-31
Processing spacing values for connector 26/27, name = con-33
Processing spacing values for connector 27/27, name = con-37
Number of unique endpoints = 17
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/27, con-1.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 2/27, con-2.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 3/27, con-3.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 4/27, con-4.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 5/27, con-5.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 6/27, con-6.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 7/27, con-7.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 8/27, con-8.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 9/27, con-9.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 10/27, con-11.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 11/27, con-13.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 12/27, con-15.
    Connector dimension changed from 6 to 8, avg. spacing changed from 16 to 11.4286
  Proximity test for connector 13/27, con-16.
    Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
  Proximity test for connector 14/27, con-17.
    Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
  Proximity test for connector 15/27, con-18.
  Proximity test for connector 16/27, con-19.
    Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
  Proximity test for connector 17/27, con-20.
    Connector dimension changed from 3 to 8, avg. spacing changed from 0.985232 to 0.281495
  Proximity test for connector 18/27, con-21.
  Proximity test for connector 19/27, con-22.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638
  Proximity test for connector 20/27, con-23.
  Proximity test for connector 21/27, con-24.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638
  Proximity test for connector 22/27, con-26.
    Connector dimension changed from 3 to 8, avg. spacing changed from 2.00803 to 0.573724
  Proximity test for connector 23/27, con-27.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656
  Proximity test for connector 24/27, con-29.
    Connector dimension changed from 3 to 8, avg. spacing changed from 1.90058 to 0.543022
  Proximity test for connector 25/27, con-31.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.47894 to 1.05638
  Proximity test for connector 26/27, con-33.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.47893 to 1.05638
  Proximity test for connector 27/27, con-37.
    Connector dimension changed from 6 to 8, avg. spacing changed from 1.63318 to 1.16656
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 8
Connector con-2 current dim = 8
Connector con-3 current dim = 8
Connector con-4 current dim = 8
Connector con-5 current dim = 8
Connector con-6 current dim = 8
Connector con-7 current dim = 8
Connector con-8 current dim = 8
Connector con-9 current dim = 8
Connector con-11 current dim = 8
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-16 current dim = 8
Connector con-17 current dim = 8
Connector con-18 current dim = 3
Connector con-19 current dim = 8
Connector con-20 current dim = 8
Connector con-21 current dim = 3
Connector con-22 current dim = 8
Connector con-23 current dim = 3
Connector con-24 current dim = 8
Connector con-26 current dim = 8
Connector con-27 current dim = 8
Connector con-29 current dim = 8
Connector con-31 current dim = 8
Connector con-33 current dim = 8
Connector con-37 current dim = 8
Domain list has 14 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 6.19964e-05
Number of periodic target domains = 0
Unstructured domain 1 of 14:
  boundary name = Farfield.
    Creating boundary name Farfield
Unstructured domain 2 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 3 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 4 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 5 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 6 of 14:
  boundary name = Farfield.
    Farfield already in boundary name list.
Unstructured domain 7 of 14:
  boundary name = Wing1.
    Creating boundary name Wing1
Unstructured domain 8 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 9 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 10 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 11 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 12 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 13 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Unstructured domain 14 of 14:
  boundary name = Wing1.
    Wing1 already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 14 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 14 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
Warning: Potential Iso Tet Boundary Recovery Problems
Warning: Out of 1262 tris, 16 have high aspect ratio.
Warning: Max. Normalized Aspect Ratio of 238: 5.06170241996981 4.27747665841954 -0.219094583351319
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:44:27PM EDT
Run Time: 00 Hours 00 Minutes 06 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:44:27PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 81 / 81 curves to EGADS originals
GMA contains 27 edge groups
GMA contains 14 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:44:28PM EDT
Export Time: 00 Hours 00 Minutes 01 Seconds
Volume mesh:
	Number of nodes          = 6967
	Number of elements       = 40421
	Number of triangles      = 1262
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 40421
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 635
	Number of elements = 1262
	Number of tris = 1262
	Number of quad = 0

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 40421
	Sideset: 'Farfield', set_id 1, num_entries 900
	Sideset: 'Wing1', set_id 2, num_entries 362
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file

ok
test_sphere (test_pointwise.TestPointwise.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
Writing global Glyph inputs...
Writing egads file '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/src/CAPS/aim/unitTest/pyCAPS/workDir_PointwiseTest/Scratch/Sphere/caps.egads'....


Running pointwise......
Number of command line arguments = 2
Tue Jun 18 2024  9:44:33PM EDT
Fidelity Pointwise 2023.2
Loading user defaults from capsUserDefaults.glf
GeomToMesh: Defaults
Connector level
    InitDim                  = 6
    MaxDim                   = 8
    MinDim                   = 3
    TurnAngle                = 0.000000
    Deviation                = 0.000000
    SplitAngle               = 0.000000
    JoinCons                 = 0
    ProxGrowthRate           = 1.300000
    SourceSpacing            = 0
    TurnAngleHard            = 70.000000
    EqualSpacing             = 0
Domain level
    Algorithm                = Delaunay
    FullLayers               = 0
    MaxLayers                = 0
    GrowthRate               = 1.300000
    IsoType                  = Triangle
    TRexType                 = Triangle
    TRexARLimit              = 200.000000
    TRexAngleBC              = 0.000000
    Decay                    = 0.500000
    MinEdge                  = 0.000000
    MaxEdge                  = 0.000000
    Adapt                    = 0
    WallSpacing              = 0.000000
    StrDomConvertARTrigger   = 0.000000
Block level
    Algorithm                = Delaunay
    VoxelLayers              = 3
    boundaryDecay            = 0.500000
    collisionBuffer          = 0.500000
    maxSkewAngle             = 180.000000
    TRexSkewDelay            = 0
    edgeMaxGrowthRate        = 1.800000
    fullLayers               = 0
    maxLayers                = 0
    growthRate               = 1.300000
    TRexType                 = TetPyramid
    volInitialize            = 1
General
    SkipMeshing              = 1
    CAESolver                = UGRID
    outerBoxScale            = 0
    sourceBoxLengthScale     = 0.000000
    sourceBoxDirection       =  1.000000 0.000000 0.000000 
    sourceBoxAngle           = 0.000000
    sourceGrowthFactor       = 10.000000
    sourcePCDFile            = 
    ModelSize                = 0
    writeGMA                 = 2.0
    assembleTolMult          = 2.0
    modelOrientIntMeshVolume = 1
Elevate On Export
    degree                   = Q1
    costThreshold            = 0.8
    maxIncAngle              = 175.0
    relax                    = 0.05
    smoothingPasses          = 1000
    WCNWeight                = 0.5
    WCNMode                  = Calculate
    writeVTU                 = false
CADFile = caps.egads
Determining model size from file.
Info: Model Size adjusted to 10
Computing maximum DB edge tolerance.
  Quilt list has 8 entries.
  Quilt quilt-1: edge tolerance = 6.91474e-06
  Quilt quilt-2: edge tolerance = 6.91474e-06
  Quilt quilt-3: edge tolerance = 5e-08
  Quilt quilt-4: edge tolerance = 5e-08
  Quilt quilt-5: edge tolerance = 5e-08
  Quilt quilt-6: edge tolerance = 5e-08
  Quilt quilt-7: edge tolerance = 5e-08
  Quilt quilt-8: edge tolerance = 5e-08
  Maximum DB edge tolerance = 6.91474e-06
Performing model assembly pass on geometry entities.
domParams(MinEdge) defined as 1.382948e-05 due to model assembly tolerance
Looking for quilt names in geometry.
  Quilt list has 8 entries.
Quilt list has 8 entries.
Original connector list has 14 entries.
Minimum connector length = 1.5708
Tolerance = 6.91474e-06
Performing merge on connectors with equal dimensions and common end points.
After regular merge, connector list has 14 entries.
Updating conData
Min Edge Tol: 5.000e-08 on con-3
Max Edge Tol: 6.915e-06 on con-1
Adjusting connector dimensions based on average spacings.
Checking dimension for connector 1/14, name = con-1
Checking dimension for connector 2/14, name = con-2
Checking dimension for connector 3/14, name = con-3
  Changing dimension for connector 3/14 from 6 to 3
Checking dimension for connector 4/14, name = con-4
  Changing dimension for connector 4/14 from 6 to 3
Checking dimension for connector 5/14, name = con-5
  Changing dimension for connector 5/14 from 6 to 3
Checking dimension for connector 6/14, name = con-6
  Changing dimension for connector 6/14 from 6 to 3
Checking dimension for connector 7/14, name = con-7
  Changing dimension for connector 7/14 from 6 to 3
Checking dimension for connector 8/14, name = con-8
  Changing dimension for connector 8/14 from 6 to 3
Checking dimension for connector 9/14, name = con-9
  Changing dimension for connector 9/14 from 6 to 3
Checking dimension for connector 10/14, name = con-10
  Changing dimension for connector 10/14 from 6 to 3
Checking dimension for connector 11/14, name = con-11
Checking dimension for connector 12/14, name = con-13
Checking dimension for connector 13/14, name = con-15
Checking dimension for connector 14/14, name = con-17
Processing spacing values for connector 1/14, name = con-1
Processing spacing values for connector 2/14, name = con-2
Processing spacing values for connector 3/14, name = con-3
Processing spacing values for connector 4/14, name = con-4
Processing spacing values for connector 5/14, name = con-5
Processing spacing values for connector 6/14, name = con-6
Processing spacing values for connector 7/14, name = con-7
Processing spacing values for connector 8/14, name = con-8
Processing spacing values for connector 9/14, name = con-9
Processing spacing values for connector 10/14, name = con-10
Processing spacing values for connector 11/14, name = con-11
Processing spacing values for connector 12/14, name = con-13
Processing spacing values for connector 13/14, name = con-15
Processing spacing values for connector 14/14, name = con-17
Number of unique endpoints = 10
Checking for baffle intersections.
Performing Local Proximity Refinement
Adjusting connector dimensions based on proximity to other connectors.
  Proximity test for connector 1/14, con-1.
  Proximity test for connector 2/14, con-2.
  Proximity test for connector 3/14, con-3.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 4/14, con-4.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 5/14, con-5.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 6/14, con-6.
    Connector dimension changed from 3 to 4, avg. spacing changed from 2 to 1.33333
  Proximity test for connector 7/14, con-7.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 8/14, con-8.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 9/14, con-9.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 10/14, con-10.
    Connector dimension changed from 3 to 5, avg. spacing changed from 2 to 1
  Proximity test for connector 11/14, con-11.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 12/14, con-13.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 13/14, con-15.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
  Proximity test for connector 14/14, con-17.
    Connector dimension changed from 6 to 8, avg. spacing changed from 3.4 to 2.42857
Adjusting node spacing from geometry
Adjusting connector dimensions based on end spacings.
Connector con-1 current dim = 6
Connector con-2 current dim = 6
Connector con-3 current dim = 4
Connector con-4 current dim = 4
Connector con-5 current dim = 4
Connector con-6 current dim = 4
Connector con-7 current dim = 5
Connector con-8 current dim = 5
Connector con-9 current dim = 5
Connector con-10 current dim = 5
Connector con-11 current dim = 8
Connector con-13 current dim = 8
Connector con-15 current dim = 8
Connector con-17 current dim = 8
Domain list has 8 entries.
Looking for periodic domain attributes from geometry.
  Tolerance = 6.91474e-06
Number of periodic target domains = 0
Unstructured domain 1 of 8:
  boundary name = sphere.
    Creating boundary name sphere
Unstructured domain 2 of 8:
  boundary name = sphere.
    sphere already in boundary name list.
Unstructured domain 3 of 8:
  boundary name = farfield.
    Creating boundary name farfield
Unstructured domain 4 of 8:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 5 of 8:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 6 of 8:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 7 of 8:
  boundary name = farfield.
    farfield already in boundary name list.
Unstructured domain 8 of 8:
  boundary name = farfield.
    farfield already in boundary name list.
Checking for blunt flag attribute on geometry faces.
Performing initialization pass on all unstructured domains.
Unstructured domain list for assembly has 8 entries.
Structured domain list for assembly has 0 entries.
Periodic target domain list for assembly has 0 entries.
Creating unstructured block from 8 domains.
Block = auto-blk
  Setting up unstructured block.
Retrieving block attributes from geometry.
  Initializing unstructured block.
CAE Solver set to UGRID
GeomToMesh finished!
Tue Jun 18 2024  9:44:37PM EDT
Run Time: 00 Hours 00 Minutes 04 Seconds
Pointwise save filename = caps.GeomToMesh.pw
Tue Jun 18 2024  9:44:37PM EDT
Exporting in UGRID format to file basename = caps.GeomToMesh
Mapped 42 / 42 curves to EGADS originals
GMA contains 14 edge groups
GMA contains 8 face groups
Wrote geometry-mesh associativity to caps.GeomToMesh.gma
GeomToMesh I/O finished!
Tue Jun 18 2024  9:44:37PM EDT
Export Time: 00 Hours 00 Minutes 00 Seconds
Volume mesh:
	Number of nodes          = 579
	Number of elements       = 2860
	Number of triangles      = 348
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 2860
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Body = 1
	Number of nodes    = 47
	Number of elements = 90
	Number of tris = 90
	Number of quad = 0
Body = 2
	Number of nodes    = 131
	Number of elements = 258
	Number of tris = 258
	Number of quad = 0
ok
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 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 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 vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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 vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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 vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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

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          = 1593
	Number of elements       = 8711
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7471
	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       = 13864
	Number of triangles      = 2758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 11106
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_boxhole (test_refine.TestREFINE.test_boxhole) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = boxhole, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 1029
	Number of elements       = 5450
	Number of triangles      = 998
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4452
	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          = 17132
	Number of elements       = 98679
	Number of triangles      = 4632
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 94047
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 94047
	Sideset: 'Farfield', set_id 1, num_entries 36
	Sideset: 'Wing1', set_id 2, num_entries 4596
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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 SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 112543
	Sideset: 'Farfield', set_id 1, num_entries 144
	Sideset: 'Wing1', set_id 2, num_entries 4422
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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 SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'Block1_tet', blk_id 1, num_entries 175654
	Sideset: 'Farfield', set_id 1, num_entries 576
	Sideset: 'Wing1', set_id 2, num_entries 5940
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing ugrid file ....
Finished writing ugrid file


Writing Tecplot file ....
Finished writing Tecplot file


Writing Binary VTK file ....
Finished writing Binary VTK 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          = 1593
	Number of elements       = 8711
	Number of triangles      = 1240
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 7471
	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          = 438
	Number of elements       = 2179
	Number of triangles      = 644
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 1535
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 1
	Name = box, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = box, index = 2
ok
test_sphere (test_refine.TestREFINE.test_sphere) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = farfield, index = 1
	Name = sphere, index = 2
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 936
	Number of elements       = 4999
	Number of triangles      = 758
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 4241
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0
ok
test_inputs (test_su2.TestSU2.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 3         
UG PARAM : mrecqm                      = 3         
UG PARAM : mpfrmt                      = 0         

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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR3    : Compile Date   03/08/24 @ 01:03AM
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          =     0.013   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6220         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1246      7333
AFLR3 IG : Nodes, Elements   =      2492     16261
AFLR3 IG : Nodes, Elements   =      3738     25021
AFLR3 IG : Nodes, Elements   =      4984     34304
AFLR3 IG : Nodes, Elements   =      6227     43518
AFLR3 IG : Nodes, Elements   =      6227     43440
AFLR3 IG : Nodes, Elements   =      6227     43475
AFLR3 IG : Nodes, Elements   =      6227     43439
AFLR3 IG : Nodes, Elements   =      6220     26110
AFLR3 IG : Nodes, Elements   =      6220     26133
AFLR3 IG : Nodes, Elements   =      6220     21491
AFLR3 IG : Nodes, Elements   =      6220     19188
 
AFLR3    : CPU Time          =     0.158   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6220     19188
AFLR3 GG : Nodes, Elements   =      9098     28027
AFLR3 GG : Nodes, Elements   =      9098     39406
AFLR3 GG : Nodes, Elements   =      9098     36704
AFLR3 GG : Nodes, Elements   =      9098     35224
AFLR3 GG : Nodes, Elements   =     11628     43169
AFLR3 GG : Nodes, Elements   =     11628     53705
AFLR3 GG : Nodes, Elements   =     11628     50685
AFLR3 GG : Nodes, Elements   =     11628     49794
AFLR3 GG : Nodes, Elements   =     14415     58408
AFLR3 GG : Nodes, Elements   =     14415     70501
AFLR3 GG : Nodes, Elements   =     14415     67147
AFLR3 GG : Nodes, Elements   =     14415     66320
AFLR3 GG : Nodes, Elements   =     17361     75337
AFLR3 GG : Nodes, Elements   =     17361     88116
AFLR3 GG : Nodes, Elements   =     17361     84624
AFLR3 GG : Nodes, Elements   =     17361     83829
AFLR3 GG : Nodes, Elements   =     20551     93587
AFLR3 GG : Nodes, Elements   =     20551    107171
AFLR3 GG : Nodes, Elements   =     20551    103485
AFLR3 GG : Nodes, Elements   =     20551    102651
AFLR3 GG : Nodes, Elements   =     23820    112676
AFLR3 GG : Nodes, Elements   =     23820    126717
AFLR3 GG : Nodes, Elements   =     23820    122888
AFLR3 GG : Nodes, Elements   =     23820    122008
AFLR3 GG : Nodes, Elements   =     27245    132431
AFLR3 GG : Nodes, Elements   =     27245    147117
AFLR3 GG : Nodes, Elements   =     27245    143166
AFLR3 GG : Nodes, Elements   =     27245    142222
AFLR3 GG : Nodes, Elements   =     30783    152976
AFLR3 GG : Nodes, Elements   =     30783    168143
AFLR3 GG : Nodes, Elements   =     30783    164070
AFLR3 GG : Nodes, Elements   =     30783    163175
AFLR3 GG : Nodes, Elements   =     34292    173827
AFLR3 GG : Nodes, Elements   =     34292    188808
AFLR3 GG : Nodes, Elements   =     34292    184786
AFLR3 GG : Nodes, Elements   =     34292    183954
AFLR3 GG : Nodes, Elements   =     37874    194791
AFLR3 GG : Nodes, Elements   =     37874    210042
AFLR3 GG : Nodes, Elements   =     37874    206016
AFLR3 GG : Nodes, Elements   =     37874    205187
AFLR3 GG : Nodes, Elements   =     41380    215779
AFLR3 GG : Nodes, Elements   =     41380    230857
AFLR3 GG : Nodes, Elements   =     41380    226861
AFLR3 GG : Nodes, Elements   =     41380    226096
AFLR3 GG : Nodes, Elements   =     44867    236615
AFLR3 GG : Nodes, Elements   =     44867    251351
AFLR3 GG : Nodes, Elements   =     44867    247508
AFLR3 GG : Nodes, Elements   =     44867    246776
AFLR3 GG : Nodes, Elements   =     48214    256863
AFLR3 GG : Nodes, Elements   =     48214    271105
AFLR3 GG : Nodes, Elements   =     48214    267402
AFLR3 GG : Nodes, Elements   =     48214    266720
AFLR3 GG : Nodes, Elements   =     51448    276453
AFLR3 GG : Nodes, Elements   =     51448    290163
AFLR3 GG : Nodes, Elements   =     51448    286615
AFLR3 GG : Nodes, Elements   =     51448    286012
AFLR3 GG : Nodes, Elements   =     54543    295326
AFLR3 GG : Nodes, Elements   =     54543    308441
AFLR3 GG : Nodes, Elements   =     54543    305058
AFLR3 GG : Nodes, Elements   =     54543    304457
AFLR3 GG : Nodes, Elements   =     57499    313335
AFLR3 GG : Nodes, Elements   =     57499    325691
AFLR3 GG : Nodes, Elements   =     57499    322594
AFLR3 GG : Nodes, Elements   =     57499    322139
AFLR3 GG : Nodes, Elements   =     60348    330690
AFLR3 GG : Nodes, Elements   =     60348    342596
AFLR3 GG : Nodes, Elements   =     60348    339582
AFLR3 GG : Nodes, Elements   =     60348    339129
AFLR3 GG : Nodes, Elements   =     63012    347124
AFLR3 GG : Nodes, Elements   =     63012    358253
AFLR3 GG : Nodes, Elements   =     63012    355484
AFLR3 GG : Nodes, Elements   =     63012    355065
AFLR3 GG : Nodes, Elements   =     65481    362480
AFLR3 GG : Nodes, Elements   =     65481    372779
AFLR3 GG : Nodes, Elements   =     65481    370210
AFLR3 GG : Nodes, Elements   =     65481    369872
AFLR3 GG : Nodes, Elements   =     67716    376581
AFLR3 GG : Nodes, Elements   =     67716    385883
AFLR3 GG : Nodes, Elements   =     67716    383531
AFLR3 GG : Nodes, Elements   =     67716    383248
AFLR3 GG : Nodes, Elements   =     69605    388917
AFLR3 GG : Nodes, Elements   =     69605    396857
AFLR3 GG : Nodes, Elements   =     69605    394794
AFLR3 GG : Nodes, Elements   =     69605    394560
AFLR3 GG : Nodes, Elements   =     71085    399002
AFLR3 GG : Nodes, Elements   =     71085    405367
AFLR3 GG : Nodes, Elements   =     71085    403587
AFLR3 GG : Nodes, Elements   =     71085    403413
AFLR3 GG : Nodes, Elements   =     72213    406798
AFLR3 GG : Nodes, Elements   =     72213    411736
AFLR3 GG : Nodes, Elements   =     72213    410308
AFLR3 GG : Nodes, Elements   =     72213    410199
AFLR3 GG : Nodes, Elements   =     73020    412620
AFLR3 GG : Nodes, Elements   =     73020    416005
AFLR3 GG : Nodes, Elements   =     73020    415096
AFLR3 GG : Nodes, Elements   =     73020    414994
AFLR3 GG : Nodes, Elements   =     73572    416650
AFLR3 GG : Nodes, Elements   =     73572    419026
AFLR3 GG : Nodes, Elements   =     73572    418352
AFLR3 GG : Nodes, Elements   =     73572    418304
AFLR3 GG : Nodes, Elements   =     73906    419306
AFLR3 GG : Nodes, Elements   =     73906    420742
AFLR3 GG : Nodes, Elements   =     73906    420326
AFLR3 GG : Nodes, Elements   =     73906    420303
AFLR3 GG : Nodes, Elements   =     74075    420811
AFLR3 GG : Nodes, Elements   =     74075    421558
AFLR3 GG : Nodes, Elements   =     74075    421311
AFLR3 GG : Nodes, Elements   =     74075    421292
AFLR3 GG : Nodes, Elements   =     74166    421565
AFLR3 GG : Nodes, Elements   =     74166    421950
AFLR3 GG : Nodes, Elements   =     74166    421833
AFLR3 GG : Nodes, Elements   =     74166    421824
AFLR3 GG : Nodes, Elements   =     74210    421956
AFLR3 GG : Nodes, Elements   =     74210    422139
AFLR3 GG : Nodes, Elements   =     74210    422074
AFLR3 GG : Nodes, Elements   =     74210    422072
AFLR3 GG : Nodes, Elements   =     74220    422102
AFLR3 GG : Nodes, Elements   =     74220    422148
AFLR3 GG : Nodes, Elements   =     74220    422135
AFLR3 GG : Nodes, Elements   =     74220    422132
AFLR3 GG : Nodes, Elements   =     74224    422144
AFLR3 GG : Nodes, Elements   =     74224    422157
AFLR3 GG : Nodes, Elements   =     74224    422154
AFLR3 GG : Nodes, Elements   =     74247    422223
AFLR3 GG : Nodes, Elements   =     74247    422312
AFLR3 GG : Nodes, Elements   =     74247    422280
AFLR3 GG : Nodes, Elements   =     74247    422279
AFLR3 GG : Nodes, Elements   =     74253    422297
AFLR3 GG : Nodes, Elements   =     74253    422323
AFLR3 GG : Nodes, Elements   =     74253    422314
AFLR3 GG : Nodes, Elements   =     74253    422312
 
AFLR3    : CPU Time          =     4.688   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     74253    422312
AFLR3 QI : Nodes, Elements   =     72809    414098
AFLR3 QI : Nodes, Elements   =     72576    412775
AFLR3 QI : Nodes, Elements   =     72556    412666
AFLR3 QI : Nodes, Elements   =     72555    412660
AFLR3 QI : Nodes, Elements   =     72555    416566
AFLR3 QI : Nodes, Elements   =     72555    412389
AFLR3 QI : Nodes, Elements   =     72555    411941
AFLR3 QI : Nodes, Elements   =     72555    412302
AFLR3 QI : Nodes, Elements   =     72555    411663
AFLR3 QI : Nodes, Elements   =     72555    411433
AFLR3 QI : Nodes, Elements   =     72555    411700
AFLR3 QI : Nodes, Elements   =     72555    411399
AFLR3 QI : Nodes, Elements   =     72555    411308
AFLR3 QI : Nodes, Elements   =     72555    411549
AFLR3 QI : Nodes, Elements   =     72555    411297
AFLR3 QI : Nodes, Elements   =     72555    411253
AFLR3 QI : Nodes, Elements   =     72555    411490
AFLR3 QI : Nodes, Elements   =     72555    411254
AFLR3 QI : Nodes, Elements   =     72555    411219
AFLR3 QI : Nodes, Elements   =     72558    411234
AFLR3 QI : Nodes, Elements   =     72558    411467
AFLR3 QI : Nodes, Elements   =     72558    411241
AFLR3 QI : Nodes, Elements   =     72558    411229
AFLR3 QI : Nodes, Elements   =     72558    411447
AFLR3 QI : Nodes, Elements   =     72558    411223
AFLR3 QI : Nodes, Elements   =     72558    411203
 
AFLR3    : CPU Time          =     1.523   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     72558    411203
AFLR3 QRG: Nodes, Elements   =     72563    411232
AFLR3 QRG: Nodes, Elements   =     72564    411237
AFLR3 QRG: Nodes, Elements   =     72568    411256
AFLR3 QRG: Nodes, Elements   =     72569    411263
 
AFLR3    : CPU Time          =     0.051   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Ang      =    0.7896     177.7
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    411263
UG3      : Min Vol           =  4.01e-10
UG3      : Average Vol       =      5.16
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     =    411263
UG3      : Min, Max Q        =    0.0428         1
UG3      : Average Q         =     0.893
UG3      : No. Q<       0.1  =        24
UG3      : No. Q<      0.01  =         0

OVERALL  : CPU Time          =     6.741   seconds

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    411263
UG3      : Min, Max Ang      =    0.7896     177.7
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        58
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      =  2.12e+06

UG3      : No. Tet Elems     =    411263
UG3      : Min Vol           =  4.01e-10
UG3      : Average Vol       =      5.16
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     =    411263
UG3      : Min, Max Q        =    0.0722         1
UG3      : Average Q         =     0.853
UG3      : No. Q<       0.1  =         1
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          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	Number of pyramids       = 0
	Number of prisms         = 0
	Number of hexahedrals    = 0

Writing SU2 file ....
Finished writing SU2 file

Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Done getting CFD boundary conditions
Writing boundary flags
 - bcProps.surfaceProp[0].surfaceType = 3
 - bcProps.surfaceProp[1].surfaceType = 1
 - bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
	Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
	Boundary condition name - Farfield
	Boundary condition name - Wing1
	Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting volume mesh

EGADS    : ---------------------------------------
EGADS    : Engineering Geometry Aircraft Design System
EGADS    : Version 1.26
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          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	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          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	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          = 72569
	Number of elements       = 423691
	Number of triangles      = 12428
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 411263
	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:62408)
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)
 7F6BD7FFF640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 7F6C6F089000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 7F6C6F089000 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
 7F6BD7FFF640 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, 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    = 296
Number of elements = 588
Number of triangle elements      = 588
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes    = 487
Number of elements = 970
Number of triangle elements      = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes    = 2048
Number of elements = 4096
Number of triangle elements      = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes    = 152
Number of elements = 300
Number of triangle elements      = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes    = 624
Number of elements = 1248
Number of triangle elements      = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes    = 488
Number of elements = 972
Number of triangle elements      = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 4193
Total number of elements = 8366
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 - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cylinder, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = cone, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = torus, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = sphere, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = boxhole, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = bullet, index = 1

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4193, elements - 8366
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    = 1352
Number of elements = 2684
Number of triangle elements      = 2684
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    = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
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 - 1352, elements - 2684
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    = 440
Number of elements = 876
Number of triangle elements      = 876
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    = 962
Total number of elements = 1920
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
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 - 440, elements - 876
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 9626, elements - 19244
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 - 7130, elements - 14252
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    = 9626
Number of elements = 19244
Number of triangle elements      = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'region_1_tet', blk_id 1, num_entries 102352
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19196
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!

Writing Binary STL file ....
Finished writing Binary STL file


Writing SU2 file ....
Finished writing SU2 file


Writing exodus file ....
	Block: 'region_1_tet', blk_id 1, num_entries 70094
	Sideset: 'Farfield', set_id 1, num_entries 48
	Sideset: 'Wing1', set_id 2, num_entries 19196
Finished writing Exodus file


Writing vtk file ....

Writing vtk general file ....
Finished writing vtk file


Writing FAST file ....
Finished writing FAST file


Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing Binary VTK file ....
Finished writing Binary VTK file

ok
test_setInput (test_tetgen.TestTETGEN.test_setInput) ...  EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_Cl (test_xfoil.Testxfoil_Kulfan.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Kulfan.test_alpha_custom_increment) ... ok
test_CL_uniform_increment (test_xfoil.Testxfoil_NACA.test_CL_uniform_increment) ... ok
test_Cl (test_xfoil.Testxfoil_NACA.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_NACA.test_alpha_custom_increment) ... ok
test_alpha_uniform_inrement (test_xfoil.Testxfoil_NACA.test_alpha_uniform_inrement) ... ok
test_append (test_xfoil.Testxfoil_NACA.test_append) ... ok
test_normalize (test_xfoil.Testxfoil_NACA.test_normalize) ... ok
test_phase (test_xfoil.Testxfoil_NACA.test_phase) ... ok
test_Output (test_zaero.TestZAERO.test_Output) ... ok
test_inputs (test_zaero.TestZAERO.test_inputs) ... Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes    = 1220
Number of elements = 2680
Number of triangle elements      = 2680
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 1221
Total number of elements = 2680
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 1
	Name = Rib_Root_Point, index = 1
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 1
	Name = Skin_Top, index = 1
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 1
	Name = Rib_Root, index = 1
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = Ribs, index = 1
	Name = Skin, index = 2
	Name = Spar1, index = 3
	Name = Rib_Root, index = 4
	Name = Spar2, index = 5
	Name = Rib_Root_Point, index = 6
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1220
	Number of elements = 2680
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 2680
	Elemental Quad4 = 0
Setting FEA Data
	Mesh for body = 1
	Number of nodal coordinates = 1
	Number of elements = 1
	Elemental Nodes = 1
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 0
Combining multiple FEA meshes!
	Combined Number of nodal coordinates = 1221
	Combined Number of elements = 2681
	Combined Elemental Nodes = 1
	Combined Elemental Rods  = 0
	Combined Elemental Tria3 = 2680
	Combined Elemental Quad4 = 0

Getting FEA materials.......
	Number of materials - 1
	Material name - madeupium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 6
	Property name - Rib_Root
	Property name - Rib_Root_Point
	Property name - Ribs
	Property name - Skin
	Property name - Spar1
	Property name - Spar2
	Done getting FEA properties
Updating mesh element types based on properties input

'Smart_Restart' is ON
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - WingSurface
	Done getting vortex lattice surface data
Getting vortex lattice control surface data
	VLM control surface name - CntrlLE
	VLM control surface name - CntrlTE
	Done getting vortex lattice control surface data

Getting FEA vortex lattice mesh

Getting ZAERO UAIC Configurations.......
	Number of UAIC Configurations - 2

	UAIC Configuration: climb, id = 1
	- Mach Number : 0.200000
	- Reduced Freq: [0.020000, ... , 0.250000]

	UAIC Configuration: cruise, id = 2
	- Mach Number : 0.700000
	- Reduced Freq: [0.040000, ... , 0.350000]

Getting ZAERO Analysis Subcases.......
	Number of Analysis Subcases - 2

	Analysis Subcase: FlutterCruise, id = 1
	- Discipline : flutter
	- UAIC       : cruise

	Analysis Subcase: Trim, id = 2
	- Discipline : Trim
	- UAIC       : climb

Getting ZAERO Trim Variables.......
	Number of Trim Variables - 2

	Trim Variable: ANGLEA
	- Label : ALPHA
	- Value : free

	Trim Variable: URDD3
	- Label : NZ
	- Value : 1.0

	Updating StaticAeroelastic subcase: Trim
	- vectorToCG -> [0.345898, 1.652951, -0.041403]
	- weight -> 476456.149985
	- weightMomentOfInertia -> [304902.643270, 98963.803820, 69822.813292, 6179.981375, 19723.152207, 370546.335524]
ok

----------------------------------------------------------------------
Ran 146 tests in 1557.019s

OK (skipped=2)
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'avlTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'awaveTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'frictionTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for 'fun3d'.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'hsm' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'interferenceTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'msesTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'mystranTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
make[1]: 'pointwiseTest' is up to date.
make[1]: Leaving directory '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/cCAPS'
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests

All tests pass!

(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)

=================================================
Using python : /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/ESP_venv/bin/python
=================================================

Running.... MINIMAL PyTests

=================================================
+ echo 'abaqus_SingleLoadCase_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
abaqus_SingleLoadCase_PyTest.py test;
+ python -u abaqus_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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    = 49
Number of elements = 36
Number of triangle elements      = 0
Number of quadrilateral elements = 36
----------------------------
Total number of nodes    = 49
Total number of elements = 36
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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 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 = 49
	Number of elements = 36
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 36

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
Analysis tuple is NULL

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - Default
	Done getting FEA analyses

Writing Abaqus grid and connectivity file ....
Finished writing Abaqus grid file


Writing Abaqus instruction file....
Writing properties
Writing materials
Writing constraints
Writing analysis (steps)


Running Abaqus......
Analysis initiated from SIMULIA established products
Abaqus JOB abaqus_CAPS
Abaqus 2023
Abaqus License Manager checked out the following licenses:
Abaqus/Standard checked out 5 tokens from Flexnet server license-4.mit.edu.
<849 out of 1100 licenses remain available>.
Abaqus Warning: Your Abaqus license will expire in 12 days.
Begin Analysis Input File Processor
Tue Jun 18 21:50:08 2024
Run pre
Tue Jun 18 21:50:09 2024
End Analysis Input File Processor
Begin Abaqus/Standard Analysis
Tue Jun 18 21:50:09 2024
Run standard
Tue Jun 18 21:50:10 2024
End Abaqus/Standard Analysis
Begin SIM Wrap-up
Tue Jun 18 21:50:10 2024
Run SMASimUtility
Tue Jun 18 21:50:10 2024
End SIM Wrap-up
Abaqus JOB abaqus_CAPS COMPLETED
Done running Abaqus!
Reading Abaqus DAT file - extracting Mises!
Reading Abaqus DAT file - extracting Displacements!
MISES =  [243147500.0, 263053750.0, 305828750.0, 328697500.0, 305828750.0, 263053750.0, 243147500.0, 429271250.0, 735352500.0, 855310000.0, 735352500.0, 429271250.0, 243147500.0, 243147500.0, 328697500.0, 328697500.0, 305828750.0, 263053750.0, 243147500.0, 429271250.0, 735352500.0, 855310000.0, 735352500.0, 429271250.0, 443783125.0, 443783125.0, 443783125.0, 443783125.0, 375120625.0, 502648750.0, 375120625.0, 617621250.0, 502648750.0, 443153750.0, 502648750.0, 443153750.0, 617621250.0, 502648750.0, 375120625.0, 405840833.3333333, 370297500.0, 438917500.0, 370297500.0, 527756250.0, 686105000.0, 527756250.0, 370297500.0, 438917500.0, 399410000.0]
Displacement =  [1.3477206e-33, 1.0531118e-33, 6.0715095e-33, 7.4429671e-33, 6.0715062e-33, 1.0531127e-33, 1.3477204e-33, 1.0265013e-32, 1.954589e-32, 2.0157204e-32, 1.9545895e-32, 1.0265011e-32, 1.3477185e-33, 1.0531096e-33, 6.0715071e-33, 7.4429667e-33, 6.0715105e-33, 1.0531132e-33, 1.3477187e-33, 1.0265012e-32, 1.9545896e-32, 2.0157204e-32, 1.9545892e-32, 1.0265015e-32, 0.0093178328, 0.0093178297, 0.0093178328, 0.0093178297, 0.0042233454, 0.0033956155, 0.004223344, 0.011896846, 0.0033956189, 0.010258672, 0.0033956155, 0.010258668, 0.011896846, 0.0033956189, 0.0042233437, 0.0042233424, 0.0015574077, 0.0053518424, 0.0015574093, 0.0036909272, 0.013167546, 0.0036909309, 0.0015574071, 0.0053518403, 0.0015574087]

real	0m4.339s
user	0m2.138s
sys	0m0.882s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case abaqus_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
CXtot   0.000611907868574681
CYtot   -6.289312383470904e-15
CZtot   -0.3012861394886091
Cltot   -4.782081713039163e-14
Cmtot   -0.1945055953450467
Cntot   -2.339461801636068e-15
Cl'tot  -4.7854363026524e-14
Cn'tot  -1.504517153549636e-15
CLtot   0.3012509314150773
CDtot   0.004646353488232845
CDvis   0.0
CLff    0.3009503023520526
CYff    -7.719145079534105e-15
CDind   0.004646353488232845
CDff    0.004968969500908293
e       0.9669902146157952
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946402, 0.0005114598078397, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080999, -0.000738653894407, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]

real	0m0.519s
user	0m0.482s
sys	0m0.370s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  [1.05475230552212, 1.36488869373643, 1.56607214272092, 2.03059709361332, 1.97271083121472, 1.87307153172173, 1.7605047576014]
Cd =  [0.0131991208675769, 0.016654024060569, 0.0200551482562873, 0.0458671341846591, 0.07542560093919, 0.0994469174479714, 0.127479430988999]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.496044114214226, 0.461377732041584, 0.442376568201776, 0.361251636069055, 0.276104140854801, 0.214381239320269, 0.132988264746769]

real	0m4.676s
user	0m4.646s
sys	0m0.368s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl =  0.37837910855492335
Cd =  0.00777585841721013
Cm =  0.0052626369958117215

real	0m4.832s
user	0m4.837s
sys	0m0.329s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]

real	0m0.334s
user	0m0.335s
sys	0m0.337s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Getting results
PAUSE Press the ENTER key to exit
To resume execution, type go.  Other input will terminate the job.
Note: The following floating-point exceptions are signalling: IEEE_OVERFLOW_FLAG IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Cl =  0.933329
Cd =  0.000283
Cd Wave =  0.0
Cm =  -0.203433
Cp _Critcal =  -1.303869

real	0m0.345s
user	0m0.366s
sys	0m0.323s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 6
	Name = 2DSlice, index = 1
	Name = TunnelWall, index = 2
	Name = OutFlow, index = 3
	Name = InFlow, index = 4
	Name = Airfoil, index = 5
	Name = AirfoilTE, index = 6

Getting mesh sizing parameters
	Mesh sizing name - Airfoil
	Mesh sizing name - AirfoilTE
	Mesh sizing name - InFlow
	Mesh sizing name - OutFlow
	Mesh sizing name - TunnelWall
	Done getting mesh sizing parameters
Getting edge discretization for body 1
	Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
	Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
	Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
	Swapping y and z coordinates!

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


Writing ugrid file ....
Finished writing ugrid file


real	0m0.649s
user	0m0.814s
sys	0m7.610s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 7
	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
	Name = Wing, index = 7
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = LeadingEdge, index = 1
	Name = TrailingEdge, index = 2

Getting mesh sizing parameters
	Mesh sizing name - LeadingEdge
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 4)
Getting surface mesh for body 2 (of 4)
Getting surface mesh for body 3 (of 4)
Getting surface mesh for body 4 (of 4)
Body 1 (of 4)
Number of nodes    = 3793
Number of elements = 4001
Number of triangle elements      = 0
Number of quadrilateral elements = 4001
Body 2 (of 4)
Number of nodes    = 1
Number of elements = 0
Number of triangle elements      = 0
Number of quadrilateral elements = 0
Body 3 (of 4)
Number of nodes    = 76
Number of elements = 55
Number of triangle elements      = 0
Number of quadrilateral elements = 55
Body 4 (of 4)
Number of nodes    = 100
Number of elements = 73
Number of triangle elements      = 0
Number of quadrilateral elements = 73
----------------------------
Total number of nodes    = 3970
Total number of elements = 4129

Writing Tecplot file ....
Finished writing Tecplot file


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid file


real	0m6.601s
user	0m29.444s
sys	1m25.789s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'aflr2_PyTest.py test;'
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
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 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          =     0.024   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          =     0.013   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


real	0m0.713s
user	0m0.817s
sys	0m1.522s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================


=================================================
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'aflr4_and_aflr3_PyTest.py test;'
aflr4_and_aflr3_PyTest.py test;
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
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


Writing ASCII STL file ....
Finished writing ASCII STL file


Writing ugrid file ....
Finished writing ugrid 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 - Wing1
	Mesh sizing name - Wing2
	Done getting mesh sizing parameters
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4    : Compile Date   04/23/24 @ 12:17PM
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          = 150512
	Number of elements       = 451696
	Number of triangles      = 14380
	Number of quadrilatarals = 0
	Number of tetrahedrals   = 216264
	Number of pyramids       = 427
	Number of prisms         = 220625
	Number of hexahedrals    = 0

Writing Tecplot file ....
Finished writing Tecplot file


real	0m16.358s
user	0m16.031s
sys	0m0.516s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes    = 2236
Number of elements = 4468
Number of triangle elements      = 4468
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes    = 636
Number of elements = 1268
Number of triangle elements      = 1268
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes    = 267
Number of elements = 530
Number of triangle elements      = 530
Number of quadrilateral elements = 0
----------------------------
Total number of nodes    = 3139
Total number of elements = 6266

Writing Tecplot file ....
Finished writing Tecplot file

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Number of surface: nodes - 3139, elements - 6266
Getting volume mesh

Generating volume mesh using TetGen.....

Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds:  0.020363
Creating surface mesh ...
Surface mesh seconds:  0.004357
Recovering boundaries...
Boundary recovery seconds:  0.043669
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds:  0.005991
Suppressing Steiner points ...
Steiner suppression seconds:  6e-06
Recovering Delaunayness...
Delaunay recovery seconds:  0.008295
Refining mesh...
  4190 insertions, added 2180 points, 134280 tetrahedra in queue.
  1395 insertions, added 459 points, 138994 tetrahedra in queue.
  1859 insertions, added 487 points, 137112 tetrahedra in queue.
  2478 insertions, added 498 points, 120303 tetrahedra in queue.
  3304 insertions, added 499 points, 74342 tetrahedra in queue.
  4404 insertions, added 474 points, 460 tetrahedra in queue.
Refinement seconds:  0.515141
Smoothing vertices...
Mesh smoothing seconds:  0.324125
Improving mesh...
Mesh improvement seconds:  0.011382
Jettisoning redundant points.

Writing nodes.
Writing elements.
Writing faces.
Writing edges.

Output seconds:  0.001782
Total running seconds:  0.935225

Statistics:

  Input points: 3139
  Input facets: 6266
  Input segments: 9399
  Input holes: 2
  Input regions: 0

  Mesh points: 8309
  Mesh tetrahedra: 41161
  Mesh faces: 85455
  Mesh faces on exterior boundary: 6266
  Mesh faces on input facets: 6266
  Mesh edges on input segments: 9399
  Steiner points inside domain: 5170

Done meshing using TetGen!

Writing Tecplot file ....
Finished writing Tecplot file


real	0m1.885s
user	0m2.062s
sys	0m0.405s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Saving geometry
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     Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2    : Compile Date   04/23/24 @ 12:17PM
AFLR2    : Copyright 1994-2021, D.L. Marcum
AFLR2    : ---------------------------------------
 
AFLR2 IC : INPUT DATA CHECK
 
AFLR2 IC : Nodes, Faces      =       545         0
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 EG : EDGE GRID RE-GENERATION
 
AFLR2 EG : Nodes, Edges      =       545       545
 
AFLR2    : CPU Time          =     0.000   seconds
 
AFLR2 IG : INITIAL GRID GENERATION
 
AFLR2 IG : Nodes, Faces      =         0         2
AFLR2 IG : Nodes, Faces      =       110       222
AFLR2 IG : Nodes, Faces      =       220       442
AFLR2 IG : Nodes, Faces      =       330       662
AFLR2 IG : Nodes, Faces      =       440       882
AFLR2 IG : Nodes, Faces      =       517      1036
AFLR2 IG : Nodes, Faces      =       545      1092
AFLR2 IG : Nodes, Faces      =       549      1092
AFLR2 IG : Nodes, Faces      =       545       545
 
AFLR2    : CPU Time          =     0.002   seconds
 
AFLR2 GG : FIELD GRID GENERATION
 
AFLR2 GGp: Nodes, Faces      =       545       545
AFLR2 GGp: Nodes, Faces      =      1083      1621
AFLR2 GGp: Nodes, Faces      =      1616      2687
AFLR2 GGp: Nodes, Faces      =      2144      3743
AFLR2 GGp: Nodes, Faces      =      2661      4777
AFLR2 GGp: Nodes, Faces      =      3171      5797
AFLR2 GGp: Nodes, Faces      =      3672      6799
AFLR2 GGp: Nodes, Faces      =      4158      7771
AFLR2 GGp: Nodes, Faces      =      4653      8761
AFLR2 GGp: Nodes, Faces      =      5142      9739
AFLR2 GGp: Nodes, Faces      =      5608     10671
AFLR2 GGp: Nodes, Faces      =      6055     11565
AFLR2 GGp: Nodes, Faces      =      6482     12419
AFLR2 GGp: Nodes, Faces      =      6880     13215
AFLR2 GGp: Nodes, Faces      =      7257     13969
AFLR2 GGp: Nodes, Faces      =      7614     14683
AFLR2 GGp: Nodes, Faces      =      7947     15349
AFLR2 GGp: Nodes, Faces      =      8276     16007
AFLR2 GGp: Nodes, Faces      =      8575     16605
AFLR2 GGp: Nodes, Faces      =      8869     17193
AFLR2 GGp: Nodes, Faces      =      9140     17735
AFLR2 GGp: Nodes, Faces      =      9401     18257
AFLR2 GGp: Nodes, Faces      =      9654     18763
AFLR2 GGp: Nodes, Faces      =      9887     19229
AFLR2 GGp: Nodes, Faces      =     10110     19675
AFLR2 GGp: Nodes, Faces      =     10315     20085
AFLR2 GGp: Nodes, Faces      =     10497     20449
AFLR2 GGp: Nodes, Faces      =     10656     20767
AFLR2 GGp: Nodes, Faces      =     10791     21037
AFLR2 GGp: Nodes, Faces      =     10919     21293
AFLR2 GGp: Nodes, Faces      =     11022     21499
AFLR2 GGp: Nodes, Faces      =     11092     21639
AFLR2 GGp: Nodes, Faces      =     11145     21745
AFLR2 GGp: Nodes, Faces      =     11156     21767
 
AFLR2    : CPU Time          =     0.038   seconds
 
AFLR2 QI : QUALITY IMPROVEMENT
 
AFLR2 QI : Nodes, Faces      =     11156     21767
AFLR2 QI : Nodes, Faces      =     11155       819
AFLR2 QI : Nodes, Faces      =     11155     10473
AFLR2 QI : Nodes, Faces      =     11155     21765
AFLR2 QI : Nodes, Faces      =     11154       811
AFLR2 QI : Nodes, Faces      =     11154     10476
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       805
AFLR2 QI : Nodes, Faces      =     11154     10479
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11154       911
AFLR2 QI : Nodes, Faces      =     11154     10426
AFLR2 QI : Nodes, Faces      =     11154     21763
AFLR2 QI : Nodes, Faces      =     11153       915
AFLR2 QI : Nodes, Faces      =     11153     10423
AFLR2 QI : Nodes, Faces      =     11153       917
AFLR2 QI : Nodes, Faces      =     11153     10423
 
AFLR2    : CPU Time          =     0.015   seconds
 
AFLR2    : DONE
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!

Writing AFLR3 file ....
Finished writing AFLR3 file

Number of nodes = 11153
Number of elements = 11885
Number of tris = 917
Number of quad = 10423
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11077 11153 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11077 complete [but 18248] (EG_makeConnect)!
EGADS Internal: Face 1, Side 10985 11152 complete [but 18249] (EG_makeConnect)!
EGADS Internal: Face 1, Side 11152 11153 complete [but 19022] (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


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

Getting CFD boundary conditions
	Boundary condition name - Airfoil
	Boundary condition name - InFlow
	Boundary condition name - OutFlow
	Boundary condition name - TunnelWall
	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......

-------------------------------------------------------------------------
|    ___ _   _ ___                                                      |
|   / __| | | |_  )   Release 8.0.0 "Harrier"                           |
|   \__ \ |_| |/ /                                                      |
|   |___/\___//___|   Suite (Computational Fluid Dynamics Code)         |
|                                                                       |
-------------------------------------------------------------------------
| SU2 Project Website: https://su2code.github.io                        |
|                                                                       |
| The SU2 Project is maintained by the SU2 Foundation                   |
| (http://su2foundation.org)                                            |
-------------------------------------------------------------------------
| Copyright 2012-2023, SU2 Contributors                                 |
|                                                                       |
| SU2 is free software; you can redistribute it and/or                  |
| modify it under the terms of the GNU Lesser General Public            |
| License as published by the Free Software Foundation; either          |
| version 2.1 of the License, or (at your option) any later version.    |
|                                                                       |
| SU2 is distributed in the hope that it will be useful,                |
| but WITHOUT ANY WARRANTY; without even the implied warranty of        |
| MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU      |
| Lesser General Public License for more details.                       |
|                                                                       |
| You should have received a copy of the GNU Lesser General Public      |
| License along with SU2. If not, see <http://www.gnu.org/licenses/>.   |
-------------------------------------------------------------------------

Parsing config file for zone 0

----------------- Physical Case Definition ( Zone 0 ) -------------------
Compressible Euler equations.
Mach number: 0.4.
Angle of attack (AoA): 0 deg, and angle of sideslip (AoS): 0 deg.
No restart solution, use the values at infinity (freestream).
Dimensional simulation.
The reference area is 1 m^2.
The semi-span will be computed using the max y(3D) value.
The reference length is 1 m.
Reference origin for moment evaluation is (0, 0, 0).
Surface(s) where the force coefficients are evaluated: BC_5.

Surface(s) plotted in the output file: BC_5, BC_2.
Input mesh file name: ../aflr2/aflr2_CAPS.su2

--------------- Space Numerical Integration ( Zone 0 ) ------------------
Roe (with entropy fix = 0.001) solver for the flow inviscid terms.
Standard Roe without low-dissipation function.
Second order integration in space, with slope limiter.
Venkatakrishnan slope-limiting method, with constant: 0.05.
The reference element size is: 1. 
Gradient for upwind reconstruction: inverse-distance weighted Least-Squares.
Gradient for viscous and source terms: inverse-distance weighted Least-Squares.

--------------- Time Numerical Integration  ( Zone 0 ) ------------------
Local time stepping (steady state simulation).
Euler implicit method for the flow equations.
FGMRES is used for solving the linear system.
Using a ILU(0) preconditioning.
Convergence criteria of the linear solver: 1e-06.
Max number of linear iterations: 10.
V Multigrid Cycle, with 2 multigrid levels.
Damping factor for the residual restriction: 0.75.
Damping factor for the correction prolongation: 0.75.
No CFL adaptation.
+-------------------------------------------+
|  MG Level| Presmooth|PostSmooth|CorrectSmo|
+-------------------------------------------+
|         0|         1|         0|         0|
|         1|         2|         0|         0|
|         2|         3|         0|         0|
+-------------------------------------------+
Courant-Friedrichs-Lewy number:       10

------------------ Convergence Criteria  ( Zone 0 ) ---------------------
Maximum number of solver subiterations: 10.
Begin convergence monitoring at iteration 5.
Residual minimum value: 1e-14.
Cauchy series min. value: 1e-10.
Number of Cauchy elements: 100.
Begin windowed time average at iteration 0.

-------------------- Output Information ( Zone 0 ) ----------------------
File writing frequency: 
+------------------------------------+
|                     File| Frequency|
+------------------------------------+
|                  RESTART|       250|
|              SURFACE_CSV|       250|
|                  TECPLOT|       250|
|          SURFACE_TECPLOT|       250|
+------------------------------------+
Writing the convergence history file every 1 inner iterations.
Writing the screen convergence history every 1 inner iterations.
The tabular file format is CSV (.csv).
Convergence history file name: history.
Forces breakdown file name: forces_breakdown_pyCAPS_su2_aflr2.dat.
Surface file name: surface_flow_pyCAPS_su2_aflr2.
Volume file name: flow_pyCAPS_su2_aflr2.
Restart file name: restart_flow_pyCAPS_su2_aflr2.dat.

------------- Config File Boundary Information ( Zone 0 ) ---------------
+-----------------------------------------------------------------------+
|                        Marker Type|                        Marker Name|
+-----------------------------------------------------------------------+
|                         Euler wall|                               BC_5|
|                                   |                               BC_2|
+-----------------------------------------------------------------------+
|                     Inlet boundary|                               BC_4|
+-----------------------------------------------------------------------+
|                    Outlet boundary|                               BC_3|
+-----------------------------------------------------------------------+

-------------------- Output Preprocessing ( Zone 0 ) --------------------

WARNING: SURFACE_PRESSURE_DROP can only be computed for at least 2 surfaces (outlet, inlet, ...)

Screen output fields: TIME_ITER, OUTER_ITER, INNER_ITER, CUR_TIME, TIME_STEP, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM-Y, RMS_ENERGY, EFFICIENCY
History output group(s): ITER, TIME_DOMAIN, WALL_TIME, RMS_RES, AERO_COEFF
Convergence field(s): RMS_DENSITY
Warning: No (valid) fields chosen for time convergence monitoring. Time convergence monitoring inactive.
Volume output fields: COORDINATES, SOLUTION, PRIMITIVE

------------------- Geometry Preprocessing ( Zone 0 ) -------------------
Two dimensional problem.
11153 grid points.
11340 volume elements.
4 surface markers.
98 boundary elements in index 0 (Marker = BC_2).
24 boundary elements in index 1 (Marker = BC_3).
24 boundary elements in index 2 (Marker = BC_4).
399 boundary elements in index 3 (Marker = BC_5).
917 triangles.
10423 quadrilaterals.
Setting point connectivity.
Renumbering points (Reverse Cuthill McKee Ordering).
Recomputing point connectivity.
Setting element connectivity.
Checking the numerical grid orientation.
There has been a re-orientation of 917 TRIANGLE volume elements.
There has been a re-orientation of 10423 QUADRILATERAL volume elements.
There has been a re-orientation of 73 LINE surface elements.
Identifying edges and vertices.
Setting the control volume structure.
Area of the computational grid: 999.878.
Searching for the closest normal neighbors to the surfaces.
Storing a mapping from global to local point index.
Compute the surface curvature.
Max K: 385.665. Mean K: 2.15881. Standard deviation K: 17.7215.
Checking for periodicity.
Computing mesh quality statistics for the dual control volumes.
+--------------------------------------------------------------+
|           Mesh Quality Metric|        Minimum|        Maximum|
+--------------------------------------------------------------+
|    Orthogonality Angle (deg.)|        49.3184|             90|
|     CV Face Area Aspect Ratio|        1.00035|        33.4982|
|           CV Sub-Volume Ratio|        1.00001|        7.89914|
+--------------------------------------------------------------+
Setting the multigrid structure.
+-------------------------------------------+
|  MG Level|       CVs|Aggl. Rate|       CFL|
+-------------------------------------------+
|         0|     11153|    1/1.00|        10|
|         1|      2702|    1/4.13|   7.38309|
|         2|       549|    1/4.92|   4.99198|
+-------------------------------------------+
Finding max control volume width.
Wetted area = 2.06265 m.
Area projection in the x-plane = 0.211192 m, y-plane = 0.997011 m.
Max. coordinate in the x-direction = 1 m, y-direction = 0.102037 m.
Min. coordinate in the x-direction = 0.000323229 m, y-direction = -0.108492 m.
Checking if Euler & Symmetry markers are straight/plane:
Boundary marker BC_5 is NOT a single straight.
Boundary marker BC_2 is NOT a single straight.
Computing wall distances.

-------------------- Solver Preprocessing ( Zone 0 ) --------------------
Inviscid flow: Computing density based on free-stream
temperature and pressure using the ideal gas law.
Force coefficients computed using free-stream values.

-- Models:
+------------------------------------------------------------------------------+
|          Viscosity Model|        Conductivity Model|              Fluid Model|
+------------------------------------------------------------------------------+
|                        -|                         -|             STANDARD_AIR|
+------------------------------------------------------------------------------+
-- Fluid properties:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|          Gas Constant|       287.058|             1|  N.m/kg.K|       287.058|
|      Spec. Heat Ratio|             -|             -|         -|           1.4|
+------------------------------------------------------------------------------+
-- Initial and free-stream conditions:
+------------------------------------------------------------------------------+
|                  Name|    Dim. value|    Ref. value|      Unit|Non-dim. value|
+------------------------------------------------------------------------------+
|       Static Pressure|        101325|             1|        Pa|        101325|
|               Density|       1.22498|             1|    kg/m^3|       1.22498|
|           Temperature|        288.15|             1|         K|        288.15|
|          Total Energy|        216054|             1|   m^2/s^2|        216054|
|            Velocity-X|       136.119|             1|       m/s|       136.119|
|            Velocity-Y|             0|             1|       m/s|             0|
|    Velocity Magnitude|       136.119|             1|       m/s|       136.119|
+------------------------------------------------------------------------------+
|           Mach Number|             -|             -|         -|           0.4|
+------------------------------------------------------------------------------+
Initialize Jacobian structure (Euler). MG level: 0.
Initialize Jacobian structure (Euler). MG level: 1.
Initialize Jacobian structure (Euler). MG level: 2.

------------------- Numerics Preprocessing ( Zone 0 ) -------------------

----------------- Integration Preprocessing ( Zone 0 ) ------------------

------------------- Iteration Preprocessing ( Zone 0 ) ------------------
Euler/Navier-Stokes/RANS fluid iteration.

------------------------------ Begin Solver -----------------------------

Simulation Run using the Single-zone Driver
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
WARNING: SU2 was not compiled for an AVX-capable architecture. Performance could be better,
         see https://su2code.github.io/docs_v7/Build-SU2-Linux-MacOS/#compiler-optimizations
+----------------------------------------------------------------------------------------------------------------------------------------------+
|   Time_Iter|  Outer_Iter|  Inner_Iter|    Cur_Time|   Time_Step|   Time(sec)|    rms[Rho]|   rms[RhoU]|   rms[RhoV]|   rms[RhoE]|        CEff|
+----------------------------------------------------------------------------------------------------------------------------------------------+
|           0|           0|           0|  0.0000e+00|  0.0000e+00|  8.2745e-02|    0.071067|    2.739763|    1.616077|    5.599701|    0.055267|
|           0|           0|           1|  0.0000e+00|  0.0000e+00|  8.1628e-02|   -0.447576|    2.193837|    1.571349|    5.070382|    0.046028|
|           0|           0|           2|  0.0000e+00|  0.0000e+00|  8.0598e-02|   -0.561159|    2.074597|    1.490746|    4.953698|    0.033910|
|           0|           0|           3|  0.0000e+00|  0.0000e+00|  7.9680e-02|   -0.723326|    1.921155|    1.390756|    4.790278|    0.049695|
|           0|           0|           4|  0.0000e+00|  0.0000e+00|  7.9106e-02|   -0.876572|    1.825653|    1.275093|    4.637161|    0.133976|
|           0|           0|           5|  0.0000e+00|  0.0000e+00|  7.8844e-02|   -1.029177|    1.759196|    1.156078|    4.482282|    0.368542|
|           0|           0|           6|  0.0000e+00|  0.0000e+00|  7.8778e-02|   -1.215334|    1.704909|    1.114966|    4.286060|    0.974759|
|           0|           0|           7|  0.0000e+00|  0.0000e+00|  7.8927e-02|   -1.329970|    1.644937|    1.145030|    4.116982|    2.716332|
|           0|           0|           8|  0.0000e+00|  0.0000e+00|  7.8936e-02|   -1.270672|    1.570739|    1.155400|    4.139480|   16.569216|
|           0|           0|           9|  0.0000e+00|  0.0000e+00|  7.9120e-02|   -1.221243|    1.499646|    1.130319|    4.189559|   -6.277653|

----------------------------- Solver Exit -------------------------------

Maximum number of iterations reached (ITER = 10) before convergence.
+-----------------------------------------------------------------------+
|      Convergence Field     |     Value    |   Criterion  |  Converged |
+-----------------------------------------------------------------------+
|                    rms[Rho]|      -1.22124|         < -14|          No|
+-----------------------------------------------------------------------+
-------------------------------------------------------------------------
+-----------------------------------------------------------------------+
|        File Writing Summary       |              Filename             |
+-----------------------------------------------------------------------+
|SU2 binary restart                 |restart_flow_pyCAPS_su2_aflr2.dat  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|CSV file                           |surface_flow_pyCAPS_su2_aflr2.csv  |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary                     |flow_pyCAPS_su2_aflr2.szplt        |

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
|Tecplot binary surface             |surface_flow_pyCAPS_su2_aflr2.szplt|
Error in tecFileWriterClose: Not all node map values for zone 1 have been written.
Currently need 994 more values.0: Error finishing Tecplot file output.

Writing the forces breakdown file (forces_breakdown_pyCAPS_su2_aflr2.dat).
+-----------------------------------------------------------------------+

--------------------------- Finalizing Solver ---------------------------
Deleted CNumerics container.
Deleted CIntegration container.
Deleted CSolver container.
Deleted CIteration container.
Deleted CInterface container.
Deleted CGeometry container.
Deleted CFreeFormDefBox class.
Deleted CSurfaceMovement class.
Deleted CVolumetricMovement class.
Deleted CConfig container.
Deleted nInst container.
Deleted COutput class.
-------------------------------------------------------------------------

------------------------- Exit Success (SU2_CFD) ------------------------

Total Force - Pressure + Viscous
Cl =  0.072253 Cd =  -0.01151
Cmz =  0.070975
Cx =  -0.01151 Cy =  0.072253
Pressure Contribution
Cl_p =  0.072253 Cd_p =  -0.01151
Cmz_p =  0.070975
Cx_p =  -0.01151 Cy_p =  0.072253
Viscous Contribution
Cl_v =  0.0 Cd_v =  0.0
Cmz_v =  0.0
Cx_v =  0.0 Cy_v =  0.0

real	0m1.985s
user	0m2.128s
sys	0m11.326s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'cart3d_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
cart3d_PyTest.py test;
+ python -u cart3d_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
 Body size = 3.796888
 Tessellating body 1 with  MaxEdge = 0.094922  Sag = 0.003797  Angle = 15.000000
 Executing: autoInputs -r 30.000000 -nDiv 6 -maxR 9  > autoInputs.out
 Executing: ./aero.csh > aero.out
C_A  0.029869406
C_Y  -0.0013620922
C_N  0.060708385
C_D  0.031969903
C_S  -0.0013620922
C_L  0.059628976
C_l  0.0472604
C_m  -0.000208726
C_n  -0.022715
C_M_x  0.0464388
C_M_y  -0.000208726
C_M_z  -0.0243505

real	0m19.458s
user	0m38.459s
sys	0m6.557s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case cart3d_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results mass properties.....

Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, 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    = 1159
Number of elements = 798
Number of triangle elements      = 0
Number of quadrilateral elements = 798
----------------------------
Total number of nodes    = 1159
Total number of elements = 798
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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_Constraint, index = 1
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 = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 1159
	Number of elements = 798
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 798

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties
Updating mesh element types based on properties input
Area      3.428666259747
Mass      5383.006027803
Centroid  [1.222256036874, 0.1634981473778, -4.234505810751e-11]
CG        [1.222256036874, 0.1634981473778, -4.234637807833e-11]
Ixx       22133.97306033
Iyy       23448.30046709
Izz       1389.213122582
Ixy       164.2055275657
Ixz       -7.45484669011e-06
Iyz       1.707686795832e-06
I         [22133.97306033, 23448.30046709, 1389.213122582, 164.2055275657, -7.45484669011e-06, 1.707686795832e-06]
II        [[22133.97306033, -164.2055275657, 7.45484669011e-06], [-164.2055275657, 23448.30046709, -1.707686795832e-06], [7.45484669011e-06, -1.707686795832e-06, 1389.213122582]]

real	0m8.295s
user	0m17.145s
sys	2m23.738s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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 capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = plate, index = 1
Creating HSM BEM
	Getting quads for BEM!
	Number of nodal coordinates = 81
	Number of elements = 96
	Elemental Tria3 = 0
	Elemental Quad4 = 64

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

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - edgeConstraint
	No "constraintType" specified for Constraint tuple edgeConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints

Getting FEA loads.......
	Number of loads - 1
	Load name - appliedPressure
	Done getting FEA loads

Writing Nastran grid and connectivity file (in small field format) ....
Finished writing Nastran grid file

Max Adjacency set to = 9
MaxDim = 32, numBCEdge = 0, numBCNode = 32, numJoint = 0
NEED TO ADD MORE CODE TO hsm_setGlobalParameter
NEED TO ADD MORE CODE TO hsm_setNodeBCParameter
NumBCNode = 32
->HSMSOL
 Matrix Non-zero Entries = 5741
 
 Converging HSM equation system ...
  iter     dr         dd         dp         rlx   max
   1    0.130E-01  0.165E+00  0.153E-04    1.000  ddy @ (   0.25   0.06   0.00)
   1*   0.260E-03  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   1*   0.240E-05  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.09   0.00)
   2    0.379E-02  0.505E-01  0.750E-04    1.000  ddy @ (   0.25   0.06   0.00)
   2*   0.420E-04  0.000E+00  0.000E+00    1.000  drz @ (   0.25   0.12   0.00)
   3    0.168E-02  0.225E-01  0.208E-04    1.000  ddy @ (   0.25   0.06   0.00)
   4    0.325E-03  0.427E-02  0.250E-05    1.000  ddy @ (   0.25   0.06   0.00)
   5    0.794E-05  0.112E-03  0.170E-06    1.000  ddy @ (   0.25   0.19   0.00)
   6    0.387E-08  0.598E-07  0.197E-09    1.000  ddy @ (   0.25   0.06   0.00)
   7    0.836E-15  0.145E-13  0.937E-15    1.000  ddy @ (   0.25   0.19   0.00)
 
 Converging n vectors ...
 it =  1    dn =  0.788E-01   rlx = 1.000  (  35 )
 it =  2    dn =  0.564E-16   rlx = 1.000  (  42 )
 
 Converging e1,e2 vectors ...
 it =  1    de =  0.691E-03   rlx = 1.000  (  45 )
 it =  2    de =  0.404E-04   rlx = 1.000  (   9 )
 it =  3    de =  0.142E-07   rlx = 1.000  (  46 )
 it =  4    de =  0.521E-11   rlx = 1.000  (  62 )
 
 Calculating  strains, stress resultants ...
Writing HSM solution to Tecplot File - HSMSingleLoadPlate.dat

real	0m1.533s
user	0m1.538s
sys	0m0.331s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================


=================================================
+ echo 'mystran_PyTest.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mystran_PyTest.py test;
+ python -u mystran_PyTest.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Getting results for natural frequencies.....
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Ribs_and_Spars, 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    = 293
Number of elements = 217
Number of triangle elements      = 0
Number of quadrilateral elements = 217
----------------------------
Total number of nodes    = 293
Total number of elements = 217
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

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_Constraint, index = 1
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 = Ribs_and_Spars, index = 1
Setting FEA Data
	Mesh for body = 0
	Number of nodal coordinates = 293
	Number of elements = 217
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 217

Getting FEA materials.......
	Number of materials - 2
	Material name - Madeupium
	Material name - Unobtainium
	No "materialType" specified for Material tuple Unobtainium, defaulting to "Isotropic"
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - Ribs_and_Spars
	No "material" specified for Property tuple Ribs_and_Spars, defaulting to an index of 1
	Done getting FEA properties

Getting FEA constraints.......
	Number of constraints - 1
	Constraint name - ribConstraint
	No "constraintType" specified for Constraint tuple ribConstraint, defaulting to "ZeroDisplacement"
	Done getting FEA constraints
Support tuple is NULL - No supports applied

Load tuple is NULL - No loads applied

Getting FEA analyses.......
	Number of analyses - 1
	Analysis name - EigenAnalysis
	No "analysisType" specified for Analysis tuple EigenAnalysis, defaulting to "Modal"
	Done getting FEA analyses

Writing Nastran grid and connectivity file (in large field format) ....
Finished writing Nastran grid file


Writing MYSTRAN instruction file....
Note: The following floating-point exceptions are signalling: IEEE_UNDERFLOW_FLAG IEEE_DENORMAL
Natural freq ( Mode 0 ) =  0.5358645270129999 (Hz)
Natural freq ( Mode 1 ) =  0.5358645288000637 (Hz)
Natural freq ( Mode 2 ) =  2.6579076333816722 (Hz)
Natural freq ( Mode 3 ) =  2.6579076480186012 (Hz)
Natural freq ( Mode 4 ) =  3.2133127087218645 (Hz)
Natural freq ( Mode 5 ) =  3.213312711432576 (Hz)
Natural freq ( Mode 6 ) =  3.7128431161841053 (Hz)
Natural freq ( Mode 7 ) =  3.7128431173689016 (Hz)
Natural freq ( Mode 8 ) =  6.903423804863681 (Hz)
Natural freq ( Mode 9 ) =  6.903423839346651 (Hz)
Natural freq ( Mode 10 ) =  8.82720702524307 (Hz)
Natural freq ( Mode 11 ) =  8.82720703135989 (Hz)
Natural freq ( Mode 12 ) =  9.03449773735593 (Hz)
Natural freq ( Mode 13 ) =  9.034497746243224 (Hz)
Natural freq ( Mode 14 ) =  12.810955940857177 (Hz)
Natural freq ( Mode 15 ) =  12.810955955283573 (Hz)
Natural freq ( Mode 16 ) =  14.595903948633964 (Hz)
Natural freq ( Mode 17 ) =  14.595903960059545 (Hz)
Natural freq ( Mode 18 ) =  17.253138348969568 (Hz)
Natural freq ( Mode 19 ) =  17.253138376627454 (Hz)
Natural freq ( Mode 20 ) =  19.538997521006213 (Hz)
Natural freq ( Mode 21 ) =  19.538997554215 (Hz)
Natural freq ( Mode 22 ) =  20.56830732889029 (Hz)
Natural freq ( Mode 23 ) =  20.568307348661286 (Hz)
Natural freq ( Mode 24 ) =  21.246868655916405 (Hz)
Natural freq ( Mode 25 ) =  21.246868660548955 (Hz)
Natural freq ( Mode 26 ) =  26.05608998380775 (Hz)
Natural freq ( Mode 27 ) =  26.05609000311102 (Hz)
Natural freq ( Mode 28 ) =  28.34916233211744 (Hz)
Natural freq ( Mode 29 ) =  28.349162400361656 (Hz)
Natural freq ( Mode 30 ) =  30.373999863572596 (Hz)
Natural freq ( Mode 31 ) =  30.3740000570112 (Hz)
Natural freq ( Mode 32 ) =  33.67251107901609 (Hz)
Natural freq ( Mode 33 ) =  33.672511087829136 (Hz)
Natural freq ( Mode 34 ) =  36.20316316648002 (Hz)
Natural freq ( Mode 35 ) =  36.20316318963648 (Hz)
Natural freq ( Mode 36 ) =  37.22279209381622 (Hz)
Natural freq ( Mode 37 ) =  37.22279210262193 (Hz)
Natural freq ( Mode 38 ) =  39.81809493912653 (Hz)
Natural freq ( Mode 39 ) =  39.81809513541885 (Hz)
Natural freq ( Mode 40 ) =  41.66707106123649 (Hz)
Natural freq ( Mode 41 ) =  41.66707106540778 (Hz)
Natural freq ( Mode 42 ) =  44.898935274249375 (Hz)
Natural freq ( Mode 43 ) =  44.89893529616552 (Hz)
Natural freq ( Mode 44 ) =  47.60456384135717 (Hz)
Natural freq ( Mode 45 ) =  47.604564003760714 (Hz)
Natural freq ( Mode 46 ) =  49.15118222293705 (Hz)
Natural freq ( Mode 47 ) =  49.15118223337741 (Hz)

real	0m10.902s
user	0m20.669s
sys	4m23.040s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case mystran_PyTest.py passed (as expected)
=================================================


=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt

Objective
---------
   -21.56250 dimensionless

Variables
---------
   x  :  1.62500   [-]   The X variable
   y  :  1.37500   [-]   The Y variable

Constants
---------
   c   :  3         [-]   A constant
   c2  :  2         [-]   A constant

Sensitivities
-------------
   c   :  + 0.46957   A constant
   c2  :  - 0.22338   A constant

Solve Report
------------
   Solve Method           :  Quadratic Program 
   Classification         :  Convex 
   Solver                 :  cvxopt 


real	0m1.746s
user	0m2.123s
sys	0m0.633s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

awave
Astros
=================================================

All tests pass!

+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort
+ mkdir -p /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/test/plugs
+ cd /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/test/plugs
+ sort -f
+ find /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/Plugs -name 'plugs0*.csm'
find: ‘/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/EngSketchPad/data/Plugs’: No such file or directory
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 31M
-rw-rw-r-- 1 jenkins jenkins 1.3M Jun 18 21:20 ASTRO.D01
-rw-rw-r-- 1 jenkins jenkins 316K Jun 18 21:20 ASTRO.IDX
-rwxrwxr-x 1 jenkins jenkins 1.1M Jun 18 21:20 avl
-rwxrwxr-x 1 jenkins jenkins  38K Jun 18 21:21 cart3dTest
-rwxrwxr-x 1 jenkins jenkins  36K Jun 18 21:19 egads2cart
-rwxrwxr-x 1 jenkins jenkins 143K Jun 18 21:21 egads2cgt
-rwxrwxr-x 1 jenkins jenkins 311K Jun 18 21:21 ESPxddm
-rwxrwxr-x 1 jenkins jenkins 689K Jun 18 21:21 friction
-rwxrwxr-x 1 jenkins jenkins 8.2M Jun 18 21:20 mastros.exe
-rwxrwxr-x 1 jenkins jenkins 727K Jun 18 21:20 mses
-rwxrwxr-x 1 jenkins jenkins 536K Jun 18 21:20 mset
-rwxrwxr-x 1 jenkins jenkins  48K Jun 18 21:20 phaseUtil
-rw-rw-r-- 1 jenkins jenkins 1.6K Jun 18 21:23 pod.egads
-rw-rw-r-- 1 jenkins jenkins    0 Jun 18 21:23 port7681.jrnl
-rwxrwxr-x 1 jenkins jenkins 451K Jun 18 21:20 pplot
-rwxrwxr-x 1 jenkins jenkins 405K Jun 18 21:20 pxplot
-rwxrwxr-x 1 jenkins jenkins 154K Jun 18 21:20 sensCSM
-rwxrwxr-x 1 jenkins jenkins 713K Jun 18 21:20 serveCSM
-rwxrwxr-x 1 jenkins jenkins 634K Jun 18 21:20 serveESP
-rwxrwxr-x 1 jenkins jenkins 731K Jun 18 21:20 Slugs
-rwxrwxr-x 1 jenkins jenkins 189K Jun 18 21:20 TestFit
-rwxrwxr-x 1 jenkins jenkins  74K Jun 18 21:19 vCurvature
-rwxrwxr-x 1 jenkins jenkins  45K Jun 18 21:19 vGeom
-rwxrwxr-x 1 jenkins jenkins  73K Jun 18 21:19 vTess
-rwxrwxr-x 1 jenkins jenkins  13M Jun 18 21:19 vTesstatic
-rw-rw-r-- 1 jenkins jenkins 195K Jun 18 21:23 wingMultiModel.bdf
-rwxrwxr-x 1 jenkins jenkins 1.1M Jun 18 21:20 xfoil
[Execution node] check if [reynolds] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [reynolds] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[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: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[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: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/jenkins/workspace/ESP_Beta/7.8/LINUX64.ifort')
[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_Beta/CASREV=7.8,ESP_ARCH=LINUX64.ifort,buildnode=reynolds #723'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS