Started by upstream project "ESP_Beta" build number 739
originally caused by:
Started by remote host 18.18.33.14
Running as SYSTEM
[EnvInject] - Loading node environment variables.
Building remotely on reynolds-centOS7 in workspace /home/jenkins/workspace/ESP_Beta/7.7/LINUX64
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
Checking out a fresh workspace because there's no workspace at /home/jenkins/workspace/ESP_Beta/7.7/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-07-26T09:46:41.139 -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 2517
Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-07-26T09:46:41.139 -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 881
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
Using sole credentials 3614a4cf-01de-4393-97de-73734b7dd5a2 in realm ‘svn+ssh://acdl.mit.edu’
[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-centOS7] is in [[macys, macys_VM, reynolds, reynolds-centOS7, reynolds-centOS8, reynolds-ubuntu18]]
Run condition [Execution node ] enabling perform for step [Execute shell]
[LINUX64] $ /bin/bash -ex /tmp/jenkins3664899600851106865.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.15
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export MPLBACKEND=agg
++ MPLBACKEND=agg
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ [[ LINUX64 == *\.\i\f\o\r\t ]]
++ '[' -f /opt/intel/oneapi/setvars.sh ']'
++ '[' -f /home/jenkins/.bashrc ']'
++ source /home/jenkins/.bashrc
+++ '[' -f /etc/bashrc ']'
+++ . /etc/bashrc
++++ '[' '' ']'
++++ shopt -q login_shell
++++ '[' 1001 -gt 199 ']'
+++++ /usr/bin/id -gn
+++++ /usr/bin/id -un
++++ '[' jenkins = jenkins ']'
++++ umask 002
++++ SHELL=/bin/bash
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/256term.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/256term.sh
+++++ local256=
+++++ '[' -n '' ']'
+++++ '[' -n '' ']'
+++++ unset local256
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/abrt-console-notification.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/abrt-console-notification.sh
+++++ tty -s
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/bash_completion.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/bash_completion.sh
+++++ '[' -z '4.2.46(2)-release' -o -z '' -o -n '' ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorgrep.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorgrep.sh
+++++ /usr/libexec/grepconf.sh -c
+++++ alias 'grep=grep --color=auto'
+++++ alias 'egrep=egrep --color=auto'
+++++ alias 'fgrep=fgrep --color=auto'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/colorls.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/colorls.sh
+++++ '[' '!' -t 0 ']'
+++++ return
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/flatpak.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/flatpak.sh
+++++ '[' /exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share = /home/jenkins/.local/share/flatpak/exports/share:/var/lib/flatpak/exports/share:/usr/local/share:/usr/share ']'
+++++ export XDG_DATA_DIRS
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/lang.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/lang.sh
+++++ sourced=0
+++++ '[' -n en_US.UTF-8 ']'
+++++ saved_lang=en_US.UTF-8
+++++ '[' -f /home/jenkins/.i18n ']'
+++++ LANG=en_US.UTF-8
+++++ unset saved_lang
+++++ '[' 0 = 1 ']'
+++++ unset sourced
+++++ unset langfile
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/less.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/less.sh
+++++ '[' -x /usr/bin/lesspipe.sh ']'
+++++ export 'LESSOPEN=||/usr/bin/lesspipe.sh %s'
+++++ LESSOPEN='||/usr/bin/lesspipe.sh %s'
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/PackageKit.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/PackageKit.sh
+++++ [[ -n '' ]]
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vim.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vim.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' -o -n '' ']'
+++++ '[' -x /usr/bin/id ']'
++++++ /usr/bin/id -u
+++++ ID=1001
+++++ '[' -n 1001 -a 1001 -le 200 ']'
+++++ alias vi
+++++ alias vi=vim
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/vte.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/vte.sh
+++++ '[' -n '4.2.46(2)-release' -o -n '' ']'
+++++ [[ ehxB == *i* ]]
+++++ return 0
++++ for i in '/etc/profile.d/*.sh'
++++ '[' -r /etc/profile.d/which2.sh ']'
++++ '[' '' ']'
++++ . /etc/profile.d/which2.sh
+++++ alias 'which=alias | /usr/bin/which --tty-only --read-alias --show-dot --show-tilde'
++++ unset i
++++ unset -f pathmunge
++ export CAPS_OUTLEVEL=0
++ CAPS_OUTLEVEL=0
++ export ESP_UDC_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/personalUdc
++ ESP_UDC_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/personalUdc
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/julia
++ export AWAVE=awavemod.f
++ AWAVE=awavemod.f
++ export RLM_CONNECT_TIMEOUT=350
++ RLM_CONNECT_TIMEOUT=350
++ [[ 7.8 != '' ]]
++ [[ '' != '' ]]
++ [[ reynolds-centOS7 == *\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:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/bin
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export EMPnumProc=4
++ EMPnumProc=4
++ export OMP_NUM_THREADS=4
++ OMP_NUM_THREADS=4
++ '[' '!' -z '' ']'
+++ ls -d /home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/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_11.5.15
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.15
++ 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:/usr/local/bin:/usr/bin
++ PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/bin
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/bin
++ [[ reynolds-centOS7 == \r\e\y\n\o\l\d\s ]]
++ 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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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:/usr/local/bin:/usr/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 ']'
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ [[ reynolds-centOS7 == \m\a\c\y\s* ]]
++ [[ reynolds-centOS7 == \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-centOS7 == \m\a\c\y\s ]]
++ [[ reynolds-centOS7 == \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=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 336ms
creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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==24.1.2, setuptools==70.1.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PATH
++ '[' x '!=' x ']'
+++ basename /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade pip
Requirement already satisfied: pip in ./ESP_venv/lib/python3.11/site-packages (24.1.2)
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-2.0.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Using cached numpy-2.0.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (19.5 MB)
Installing collected packages: numpy
Successfully installed numpy-2.0.1
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.34.2-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-1.14.0-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-2024.7.4-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-1.14.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (41.1 MB)
Using cached certifi-2024.7.4-py3-none-any.whl (162 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 2.0.1
Uninstalling numpy-2.0.1:
Successfully uninstalled numpy-2.0.1
Successfully installed certifi-2024.7.4 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 numpy-1.26.4 openmdao-3.34.2 packaging-24.1 requests-2.32.3 scipy-1.14.0 urllib3-2.2.2
+ [[ reynolds-centOS7 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.1-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-4.53.1-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-10.4.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_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-3.9.1-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-4.53.1-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-10.4.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_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-4.53.1 kiwisolver-1.4.5 matplotlib-3.9.1 pillow-10.4.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade scipy
Requirement already satisfied: scipy in ./ESP_venv/lib/python3.11/site-packages (1.14.0)
Requirement already satisfied: numpy<2.3,>=1.23.5 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
--2024-07-26 09:47:26-- 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: 271882371 (259M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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1600K .......... .......... .......... .......... .......... 0% 35.3M 8s
1650K .......... .......... .......... .......... .......... 0% 46.4M 8s
1700K .......... .......... .......... .......... .......... 0% 22.0M 8s
1750K .......... .......... .......... .......... .......... 0% 55.9M 8s
1800K .......... .......... .......... .......... .......... 0% 38.3M 8s
1850K .......... .......... .......... .......... .......... 0% 44.4M 8s
1900K .......... .......... .......... .......... .......... 0% 37.2M 8s
1950K .......... .......... .......... .......... .......... 0% 29.6M 8s
2000K .......... .......... .......... .......... .......... 0% 33.1M 8s
2050K .......... .......... .......... .......... .......... 0% 45.4M 8s
2100K .......... .......... .......... .......... .......... 0% 29.5M 8s
2150K .......... .......... .......... .......... .......... 0% 54.9M 8s
2200K .......... .......... .......... .......... .......... 0% 45.7M 8s
2250K .......... .......... .......... .......... .......... 0% 32.2M 8s
2300K .......... .......... .......... .......... .......... 0% 34.8M 8s
2350K .......... .......... .......... .......... .......... 0% 50.4M 8s
2400K .......... .......... .......... .......... .......... 0% 109M 7s
2450K .......... .......... .......... .......... .......... 0% 35.2M 7s
2500K .......... .......... .......... .......... .......... 0% 92.0M 7s
2550K .......... .......... .......... .......... .......... 0% 43.3M 7s
2600K .......... .......... .......... .......... .......... 0% 45.3M 7s
2650K .......... .......... .......... .......... .......... 1% 44.1M 7s
2700K .......... .......... .......... .......... .......... 1% 31.3M 7s
2750K .......... .......... .......... .......... .......... 1% 28.0M 7s
2800K .......... .......... .......... .......... .......... 1% 53.0M 7s
2850K .......... .......... .......... .......... .......... 1% 46.3M 7s
2900K .......... .......... .......... .......... .......... 1% 43.3M 7s
2950K .......... .......... .......... .......... .......... 1% 23.8M 7s
3000K .......... .......... .......... .......... .......... 1% 36.8M 7s
3050K .......... .......... .......... .......... .......... 1% 28.9M 7s
3100K .......... .......... .......... .......... .......... 1% 30.6M 7s
3150K .......... .......... .......... .......... .......... 1% 40.0M 7s
3200K .......... .......... .......... .......... .......... 1% 49.2M 7s
3250K .......... .......... .......... .......... .......... 1% 41.1M 7s
3300K .......... .......... .......... .......... .......... 1% 60.4M 7s
3350K .......... .......... .......... .......... .......... 1% 30.9M 7s
3400K .......... .......... .......... .......... .......... 1% 60.5M 7s
3450K .......... .......... .......... .......... .......... 1% 45.7M 7s
3500K .......... .......... .......... .......... .......... 1% 38.3M 7s
3550K .......... .......... .......... .......... .......... 1% 67.8M 7s
3600K .......... .......... .......... .......... .......... 1% 24.5M 7s
3650K .......... .......... .......... .......... .......... 1% 74.1M 7s
3700K .......... .......... .......... .......... .......... 1% 39.8M 7s
3750K .......... .......... .......... .......... .......... 1% 43.7M 7s
3800K .......... .......... .......... .......... .......... 1% 69.4M 7s
3850K .......... .......... .......... .......... .......... 1% 51.1M 7s
3900K .......... .......... .......... .......... .......... 1% 137M 7s
3950K .......... .......... .......... .......... .......... 1% 38.0M 7s
4000K .......... .......... .......... .......... .......... 1% 85.9M 7s
4050K .......... .......... .......... .......... .......... 1% 97.1M 7s
4100K .......... .......... .......... .......... .......... 1% 25.4M 7s
4150K .......... .......... .......... .......... .......... 1% 62.8M 7s
4200K .......... .......... .......... .......... .......... 1% 27.9M 7s
4250K .......... .......... .......... .......... .......... 1% 68.1M 7s
4300K .......... .......... .......... .......... .......... 1% 53.8M 7s
4350K .......... .......... .......... .......... .......... 1% 40.0M 7s
4400K .......... .......... .......... .......... .......... 1% 46.2M 7s
4450K .......... .......... .......... .......... .......... 1% 43.5M 7s
4500K .......... .......... .......... .......... .......... 1% 94.4M 7s
4550K .......... .......... .......... .......... .......... 1% 58.9M 7s
4600K .......... .......... .......... .......... .......... 1% 63.0M 7s
4650K .......... .......... .......... .......... .......... 1% 40.9M 7s
4700K .......... .......... .......... .......... .......... 1% 51.3M 7s
4750K .......... .......... .......... .......... .......... 1% 43.7M 7s
4800K .......... .......... .......... .......... .......... 1% 72.8M 7s
4850K .......... .......... .......... .......... .......... 1% 52.3M 7s
4900K .......... .......... .......... .......... .......... 1% 97.7M 7s
4950K .......... .......... .......... .......... .......... 1% 34.7M 7s
5000K .......... .......... .......... .......... .......... 1% 65.6M 6s
5050K .......... .......... .......... .......... .......... 1% 60.2M 6s
5100K .......... .......... .......... .......... .......... 1% 31.5M 6s
5150K .......... .......... .......... .......... .......... 1% 151M 6s
5200K .......... .......... .......... .......... .......... 1% 108M 6s
5250K .......... .......... .......... .......... .......... 1% 37.0M 6s
5300K .......... .......... .......... .......... .......... 2% 48.2M 6s
5350K .......... .......... .......... .......... .......... 2% 53.6M 6s
5400K .......... .......... .......... .......... .......... 2% 121M 6s
5450K .......... .......... .......... .......... .......... 2% 98.4M 6s
5500K .......... .......... .......... .......... .......... 2% 92.0M 6s
5550K .......... .......... .......... .......... .......... 2% 237M 6s
5600K .......... .......... .......... .......... .......... 2% 167M 6s
5650K .......... .......... .......... .......... .......... 2% 197M 6s
5700K .......... .......... .......... .......... .......... 2% 6.52M 6s
5750K .......... .......... .......... .......... .......... 2% 17.0M 6s
5800K .......... .......... .......... .......... .......... 2% 40.3M 6s
5850K .......... .......... .......... .......... .......... 2% 33.2M 6s
5900K .......... .......... .......... .......... .......... 2% 175M 6s
5950K .......... .......... .......... .......... .......... 2% 44.5M 6s
6000K .......... .......... .......... .......... .......... 2% 45.5M 6s
6050K .......... .......... .......... .......... .......... 2% 40.0M 6s
6100K .......... .......... .......... .......... .......... 2% 34.0M 6s
6150K .......... .......... .......... .......... .......... 2% 118M 6s
6200K .......... .......... .......... .......... .......... 2% 74.0M 6s
6250K .......... .......... .......... .......... .......... 2% 60.0M 6s
6300K .......... .......... .......... .......... .......... 2% 220M 6s
6350K .......... .......... .......... .......... .......... 2% 60.3M 6s
6400K .......... .......... .......... .......... .......... 2% 137M 6s
6450K .......... .......... .......... .......... .......... 2% 63.5M 6s
6500K .......... .......... .......... .......... .......... 2% 162M 6s
6550K .......... .......... .......... .......... .......... 2% 48.3M 6s
6600K .......... .......... .......... .......... .......... 2% 77.5M 6s
6650K .......... .......... .......... .......... .......... 2% 73.0M 6s
6700K .......... .......... .......... .......... .......... 2% 172M 6s
6750K .......... .......... .......... .......... .......... 2% 49.7M 6s
6800K .......... .......... .......... .......... .......... 2% 216M 6s
6850K .......... .......... .......... .......... .......... 2% 55.6M 6s
6900K .......... .......... .......... .......... .......... 2% 60.2M 6s
6950K .......... .......... .......... .......... .......... 2% 36.8M 6s
7000K .......... .......... .......... .......... .......... 2% 38.9M 6s
7050K .......... .......... .......... .......... .......... 2% 42.5M 6s
7100K .......... .......... .......... .......... .......... 2% 103M 6s
7150K .......... .......... .......... .......... .......... 2% 33.2M 6s
7200K .......... .......... .......... .......... .......... 2% 37.9M 6s
7250K .......... .......... .......... .......... .......... 2% 34.3M 6s
7300K .......... .......... .......... .......... .......... 2% 36.0M 6s
7350K .......... .......... .......... .......... .......... 2% 82.5M 6s
7400K .......... .......... .......... .......... .......... 2% 30.1M 6s
7450K .......... .......... .......... .......... .......... 2% 40.4M 6s
7500K .......... .......... .......... .......... .......... 2% 30.9M 6s
7550K .......... .......... .......... .......... .......... 2% 40.3M 6s
7600K .......... .......... .......... .......... .......... 2% 64.2M 6s
7650K .......... .......... .......... .......... .......... 2% 43.4M 6s
7700K .......... .......... .......... .......... .......... 2% 31.5M 6s
7750K .......... .......... .......... .......... .......... 2% 31.9M 6s
7800K .......... .......... .......... .......... .......... 2% 124M 6s
7850K .......... .......... .......... .......... .......... 2% 36.8M 6s
7900K .......... .......... .......... .......... .......... 2% 41.9M 6s
7950K .......... .......... .......... .......... .......... 3% 35.1M 6s
8000K .......... .......... .......... .......... .......... 3% 45.3M 6s
8050K .......... .......... .......... .......... .......... 3% 177M 6s
8100K .......... .......... .......... .......... .......... 3% 34.2M 6s
8150K .......... .......... .......... .......... .......... 3% 34.3M 6s
8200K .......... .......... .......... .......... .......... 3% 33.0M 6s
8250K .......... .......... .......... .......... .......... 3% 82.0M 6s
8300K .......... .......... .......... .......... .......... 3% 87.7M 6s
8350K .......... .......... .......... .......... .......... 3% 27.8M 6s
8400K .......... .......... .......... .......... .......... 3% 59.1M 6s
8450K .......... .......... .......... .......... .......... 3% 5.92M 6s
8500K .......... .......... .......... .......... .......... 3% 251M 6s
8550K .......... .......... .......... .......... .......... 3% 73.1M 6s
8600K .......... .......... .......... .......... .......... 3% 43.9M 6s
8650K .......... .......... .......... .......... .......... 3% 79.5M 6s
8700K .......... .......... .......... .......... .......... 3% 22.9M 6s
8750K .......... .......... .......... .......... .......... 3% 53.0M 6s
8800K .......... .......... .......... .......... .......... 3% 87.6M 6s
8850K .......... .......... .......... .......... .......... 3% 51.4M 6s
8900K .......... .......... .......... .......... .......... 3% 60.4M 6s
8950K .......... .......... .......... .......... .......... 3% 68.7M 6s
9000K .......... .......... .......... .......... .......... 3% 86.5M 6s
9050K .......... .......... .......... .......... .......... 3% 43.8M 6s
9100K .......... .......... .......... .......... .......... 3% 76.1M 6s
9150K .......... .......... .......... .......... .......... 3% 55.2M 6s
9200K .......... .......... .......... .......... .......... 3% 101M 6s
9250K .......... .......... .......... .......... .......... 3% 119M 6s
9300K .......... .......... .......... .......... .......... 3% 27.6M 6s
9350K .......... .......... .......... .......... .......... 3% 72.2M 6s
9400K .......... .......... .......... .......... .......... 3% 83.7M 6s
9450K .......... .......... .......... .......... .......... 3% 78.3M 6s
9500K .......... .......... .......... .......... .......... 3% 7.60M 6s
9550K .......... .......... .......... .......... .......... 3% 28.0M 6s
9600K .......... .......... .......... .......... .......... 3% 59.1M 6s
9650K .......... .......... .......... .......... .......... 3% 20.8M 6s
9700K .......... .......... .......... .......... .......... 3% 67.7M 6s
9750K .......... .......... .......... .......... .......... 3% 180M 6s
9800K .......... .......... .......... .......... .......... 3% 132M 6s
9850K .......... .......... .......... .......... .......... 3% 54.0M 6s
9900K .......... .......... .......... .......... .......... 3% 197M 6s
9950K .......... .......... .......... .......... .......... 3% 227M 6s
10000K .......... .......... .......... .......... .......... 3% 175M 6s
10050K .......... .......... .......... .......... .......... 3% 58.5M 6s
10100K .......... .......... .......... .......... .......... 3% 31.1M 6s
10150K .......... .......... .......... .......... .......... 3% 69.5M 6s
10200K .......... .......... .......... .......... .......... 3% 30.7M 6s
10250K .......... .......... .......... .......... .......... 3% 27.7M 6s
10300K .......... .......... .......... .......... .......... 3% 31.0M 6s
10350K .......... .......... .......... .......... .......... 3% 33.2M 6s
10400K .......... .......... .......... .......... .......... 3% 55.6M 6s
10450K .......... .......... .......... .......... .......... 3% 11.8M 6s
10500K .......... .......... .......... .......... .......... 3% 49.3M 6s
10550K .......... .......... .......... .......... .......... 3% 97.6M 6s
10600K .......... .......... .......... .......... .......... 4% 75.2M 6s
10650K .......... .......... .......... .......... .......... 4% 3.93M 6s
10700K .......... .......... .......... .......... .......... 4% 44.6M 6s
10750K .......... .......... .......... .......... .......... 4% 121M 6s
10800K .......... .......... .......... .......... .......... 4% 38.1M 6s
10850K .......... .......... .......... .......... .......... 4% 76.5M 6s
10900K .......... .......... .......... .......... .......... 4% 76.6M 6s
10950K .......... .......... .......... .......... .......... 4% 65.0M 6s
11000K .......... .......... .......... .......... .......... 4% 16.0M 6s
11050K .......... .......... .......... .......... .......... 4% 67.4M 6s
11100K .......... .......... .......... .......... .......... 4% 23.6M 6s
11150K .......... .......... .......... .......... .......... 4% 53.3M 6s
11200K .......... .......... .......... .......... .......... 4% 90.3M 6s
11250K .......... .......... .......... .......... .......... 4% 41.3M 6s
11300K .......... .......... .......... .......... .......... 4% 18.2M 6s
11350K .......... .......... .......... .......... .......... 4% 100M 6s
11400K .......... .......... .......... .......... .......... 4% 19.5M 6s
11450K .......... .......... .......... .......... .......... 4% 25.5M 6s
11500K .......... .......... .......... .......... .......... 4% 32.2M 6s
11550K .......... .......... .......... .......... .......... 4% 41.1M 6s
11600K .......... .......... .......... .......... .......... 4% 26.4M 6s
11650K .......... .......... .......... .......... .......... 4% 45.5M 6s
11700K .......... .......... .......... .......... .......... 4% 25.0M 6s
11750K .......... .......... .......... .......... .......... 4% 20.3M 6s
11800K .......... .......... .......... .......... .......... 4% 93.6M 6s
11850K .......... .......... .......... .......... .......... 4% 14.2M 6s
11900K .......... .......... .......... .......... .......... 4% 20.1M 6s
11950K .......... .......... .......... .......... .......... 4% 17.0M 6s
12000K .......... .......... .......... .......... .......... 4% 41.7M 6s
12050K .......... .......... .......... .......... .......... 4% 174M 6s
12100K .......... .......... .......... .......... .......... 4% 8.00M 7s
12150K .......... .......... .......... .......... .......... 4% 48.5M 7s
12200K .......... .......... .......... .......... .......... 4% 88.9M 7s
12250K .......... .......... .......... .......... .......... 4% 106M 6s
12300K .......... .......... .......... .......... .......... 4% 173M 6s
12350K .......... .......... .......... .......... .......... 4% 10.2M 7s
12400K .......... .......... .......... .......... .......... 4% 45.7M 7s
12450K .......... .......... .......... .......... .......... 4% 91.3M 7s
12500K .......... .......... .......... .......... .......... 4% 19.2M 7s
12550K .......... .......... .......... .......... .......... 4% 71.2M 7s
12600K .......... .......... .......... .......... .......... 4% 91.3M 7s
12650K .......... .......... .......... .......... .......... 4% 46.6M 6s
12700K .......... .......... .......... .......... .......... 4% 5.10M 7s
12750K .......... .......... .......... .......... .......... 4% 22.3M 7s
12800K .......... .......... .......... .......... .......... 4% 94.8M 7s
12850K .......... .......... .......... .......... .......... 4% 113M 7s
12900K .......... .......... .......... .......... .......... 4% 103M 7s
12950K .......... .......... .......... .......... .......... 4% 47.3M 7s
13000K .......... .......... .......... .......... .......... 4% 159M 7s
13050K .......... .......... .......... .......... .......... 4% 40.4M 7s
13100K .......... .......... .......... .......... .......... 4% 21.6M 7s
13150K .......... .......... .......... .......... .......... 4% 20.8M 7s
13200K .......... .......... .......... .......... .......... 4% 6.15M 7s
13250K .......... .......... .......... .......... .......... 5% 206M 7s
13300K .......... .......... .......... .......... .......... 5% 19.8M 7s
13350K .......... .......... .......... .......... .......... 5% 27.0M 7s
13400K .......... .......... .......... .......... .......... 5% 201M 7s
13450K .......... .......... .......... .......... .......... 5% 20.8M 7s
13500K .......... .......... .......... .......... .......... 5% 6.59M 7s
13550K .......... .......... .......... .......... .......... 5% 164M 7s
13600K .......... .......... .......... .......... .......... 5% 14.7M 7s
13650K .......... .......... .......... .......... .......... 5% 131M 7s
13700K .......... .......... .......... .......... .......... 5% 14.3M 7s
13750K .......... .......... .......... .......... .......... 5% 18.3M 7s
13800K .......... .......... .......... .......... .......... 5% 14.1M 7s
13850K .......... .......... .......... .......... .......... 5% 10.3M 7s
13900K .......... .......... .......... .......... .......... 5% 15.1M 7s
13950K .......... .......... .......... .......... .......... 5% 13.5M 7s
14000K .......... .......... .......... .......... .......... 5% 14.0M 7s
14050K .......... .......... .......... .......... .......... 5% 13.3M 7s
14100K .......... .......... .......... .......... .......... 5% 3.23M 7s
14150K .......... .......... .......... .......... .......... 5% 192M 7s
14200K .......... .......... .......... .......... .......... 5% 219M 7s
14250K .......... .......... .......... .......... .......... 5% 4.15M 8s
14300K .......... .......... .......... .......... .......... 5% 228M 8s
14350K .......... .......... .......... .......... .......... 5% 210M 7s
14400K .......... .......... .......... .......... .......... 5% 15.9M 8s
14450K .......... .......... .......... .......... .......... 5% 13.1M 8s
14500K .......... .......... .......... .......... .......... 5% 13.4M 8s
14550K .......... .......... .......... .......... .......... 5% 8.39M 8s
14600K .......... .......... .......... .......... .......... 5% 14.1M 8s
14650K .......... .......... .......... .......... .......... 5% 12.8M 8s
14700K .......... .......... .......... .......... .......... 5% 15.1M 8s
14750K .......... .......... .......... .......... .......... 5% 15.3M 8s
14800K .......... .......... .......... .......... .......... 5% 14.7M 8s
14850K .......... .......... .......... .......... .......... 5% 13.0M 8s
14900K .......... .......... .......... .......... .......... 5% 16.7M 8s
14950K .......... .......... .......... .......... .......... 5% 13.8M 8s
15000K .......... .......... .......... .......... .......... 5% 14.6M 8s
15050K .......... .......... .......... .......... .......... 5% 5.62M 8s
15100K .......... .......... .......... .......... .......... 5% 68.9M 8s
15150K .......... .......... .......... .......... .......... 5% 17.0M 8s
15200K .......... .......... .......... .......... .......... 5% 11.6M 8s
15250K .......... .......... .......... .......... .......... 5% 13.2M 8s
15300K .......... .......... .......... .......... .......... 5% 17.0M 8s
15350K .......... .......... .......... .......... .......... 5% 10.2M 8s
15400K .......... .......... .......... .......... .......... 5% 17.5M 8s
15450K .......... .......... .......... .......... .......... 5% 9.56M 8s
15500K .......... .......... .......... .......... .......... 5% 7.82M 8s
15550K .......... .......... .......... .......... .......... 5% 19.4M 8s
15600K .......... .......... .......... .......... .......... 5% 9.86M 8s
15650K .......... .......... .......... .......... .......... 5% 8.10M 8s
15700K .......... .......... .......... .......... .......... 5% 6.05M 9s
15750K .......... .......... .......... .......... .......... 5% 9.69M 9s
15800K .......... .......... .......... .......... .......... 5% 15.3M 9s
15850K .......... .......... .......... .......... .......... 5% 7.76M 9s
15900K .......... .......... .......... .......... .......... 6% 9.41M 9s
15950K .......... .......... .......... .......... .......... 6% 9.68M 9s
16000K .......... .......... .......... .......... .......... 6% 10.4M 9s
16050K .......... .......... .......... .......... .......... 6% 17.2M 9s
16100K .......... .......... .......... .......... .......... 6% 16.8M 9s
16150K .......... .......... .......... .......... .......... 6% 8.03M 9s
16200K .......... .......... .......... .......... .......... 6% 17.9M 9s
16250K .......... .......... .......... .......... .......... 6% 14.7M 9s
16300K .......... .......... .......... .......... .......... 6% 7.54M 9s
16350K .......... .......... .......... .......... .......... 6% 13.1M 9s
16400K .......... .......... .......... .......... .......... 6% 11.5M 9s
16450K .......... .......... .......... .......... .......... 6% 10.0M 9s
16500K .......... .......... .......... .......... .......... 6% 15.1M 9s
16550K .......... .......... .......... .......... .......... 6% 8.36M 9s
16600K .......... .......... .......... .......... .......... 6% 9.09M 9s
16650K .......... .......... .......... .......... .......... 6% 12.7M 9s
16700K .......... .......... .......... .......... .......... 6% 7.34M 9s
16750K .......... .......... .......... .......... .......... 6% 11.4M 9s
16800K .......... .......... .......... .......... .......... 6% 11.9M 9s
16850K .......... .......... .......... .......... .......... 6% 9.49M 9s
16900K .......... .......... .......... .......... .......... 6% 12.6M 10s
16950K .......... .......... .......... .......... .......... 6% 9.14M 10s
17000K .......... .......... .......... .......... .......... 6% 9.04M 10s
17050K .......... .......... .......... .......... .......... 6% 11.9M 10s
17100K .......... .......... .......... .......... .......... 6% 8.36M 10s
17150K .......... .......... .......... .......... .......... 6% 11.4M 10s
17200K .......... .......... .......... .......... .......... 6% 10.2M 10s
17250K .......... .......... .......... .......... .......... 6% 12.6M 10s
17300K .......... .......... .......... .......... .......... 6% 12.3M 10s
17350K .......... .......... .......... .......... .......... 6% 10.5M 10s
17400K .......... .......... .......... .......... .......... 6% 10.8M 10s
17450K .......... .......... .......... .......... .......... 6% 10.5M 10s
17500K .......... .......... .......... .......... .......... 6% 9.78M 10s
17550K .......... .......... .......... .......... .......... 6% 6.29M 10s
17600K .......... .......... .......... .......... .......... 6% 79.7M 10s
17650K .......... .......... .......... .......... .......... 6% 9.57M 10s
17700K .......... .......... .......... .......... .......... 6% 8.53M 10s
17750K .......... .......... .......... .......... .......... 6% 12.3M 10s
17800K .......... .......... .......... .......... .......... 6% 8.59M 10s
17850K .......... .......... .......... .......... .......... 6% 13.1M 10s
17900K .......... .......... .......... .......... .......... 6% 8.56M 10s
17950K .......... .......... .......... .......... .......... 6% 8.42M 10s
18000K .......... .......... .......... .......... .......... 6% 11.2M 10s
18050K .......... .......... .......... .......... .......... 6% 12.1M 10s
18100K .......... .......... .......... .......... .......... 6% 10.9M 10s
18150K .......... .......... .......... .......... .......... 6% 8.30M 10s
18200K .......... .......... .......... .......... .......... 6% 9.22M 10s
18250K .......... .......... .......... .......... .......... 6% 13.2M 10s
18300K .......... .......... .......... .......... .......... 6% 12.0M 11s
18350K .......... .......... .......... .......... .......... 6% 10.4M 11s
18400K .......... .......... .......... .......... .......... 6% 10.5M 11s
18450K .......... .......... .......... .......... .......... 6% 12.9M 11s
18500K .......... .......... .......... .......... .......... 6% 12.1M 11s
18550K .......... .......... .......... .......... .......... 7% 11.5M 11s
18600K .......... .......... .......... .......... .......... 7% 13.0M 11s
18650K .......... .......... .......... .......... .......... 7% 23.8M 11s
18700K .......... .......... .......... .......... .......... 7% 7.94M 11s
18750K .......... .......... .......... .......... .......... 7% 8.81M 11s
18800K .......... .......... .......... .......... .......... 7% 18.0M 11s
18850K .......... .......... .......... .......... .......... 7% 8.07M 11s
18900K .......... .......... .......... .......... .......... 7% 19.5M 11s
18950K .......... .......... .......... .......... .......... 7% 11.7M 11s
19000K .......... .......... .......... .......... .......... 7% 12.7M 11s
19050K .......... .......... .......... .......... .......... 7% 11.5M 11s
19100K .......... .......... .......... .......... .......... 7% 13.4M 11s
19150K .......... .......... .......... .......... .......... 7% 11.1M 11s
19200K .......... .......... .......... .......... .......... 7% 14.2M 11s
19250K .......... .......... .......... .......... .......... 7% 11.1M 11s
19300K .......... .......... .......... .......... .......... 7% 17.0M 11s
19350K .......... .......... .......... .......... .......... 7% 12.3M 11s
19400K .......... .......... .......... .......... .......... 7% 19.6M 11s
19450K .......... .......... .......... .......... .......... 7% 13.8M 11s
19500K .......... .......... .......... .......... .......... 7% 10.1M 11s
19550K .......... .......... .......... .......... .......... 7% 15.6M 11s
19600K .......... .......... .......... .......... .......... 7% 6.97M 11s
19650K .......... .......... .......... .......... .......... 7% 55.0M 11s
19700K .......... .......... .......... .......... .......... 7% 8.45M 11s
19750K .......... .......... .......... .......... .......... 7% 14.5M 11s
19800K .......... .......... .......... .......... .......... 7% 10.7M 11s
19850K .......... .......... .......... .......... .......... 7% 5.89M 11s
19900K .......... .......... .......... .......... .......... 7% 8.06M 11s
19950K .......... .......... .......... .......... .......... 7% 6.09M 11s
20000K .......... .......... .......... .......... .......... 7% 8.53M 11s
20050K .......... .......... .......... .......... .......... 7% 6.87M 11s
20100K .......... .......... .......... .......... .......... 7% 9.81M 11s
20150K .......... .......... .......... .......... .......... 7% 6.03M 12s
20200K .......... .......... .......... .......... .......... 7% 8.38M 12s
20250K .......... .......... .......... .......... .......... 7% 9.49M 12s
20300K .......... .......... .......... .......... .......... 7% 6.71M 12s
20350K .......... .......... .......... .......... .......... 7% 11.6M 12s
20400K .......... .......... .......... .......... .......... 7% 11.4M 12s
20450K .......... .......... .......... .......... .......... 7% 5.82M 12s
20500K .......... .......... .......... .......... .......... 7% 11.6M 12s
20550K .......... .......... .......... .......... .......... 7% 6.79M 12s
20600K .......... .......... .......... .......... .......... 7% 5.99M 12s
20650K .......... .......... .......... .......... .......... 7% 10.6M 12s
20700K .......... .......... .......... .......... .......... 7% 5.84M 12s
20750K .......... .......... .......... .......... .......... 7% 5.57M 12s
20800K .......... .......... .......... .......... .......... 7% 6.72M 12s
20850K .......... .......... .......... .......... .......... 7% 6.07M 12s
20900K .......... .......... .......... .......... .......... 7% 4.42M 12s
20950K .......... .......... .......... .......... .......... 7% 4.35M 12s
21000K .......... .......... .......... .......... .......... 7% 6.71M 12s
21050K .......... .......... .......... .......... .......... 7% 4.61M 13s
21100K .......... .......... .......... .......... .......... 7% 7.11M 13s
21150K .......... .......... .......... .......... .......... 7% 7.28M 13s
21200K .......... .......... .......... .......... .......... 8% 7.02M 13s
21250K .......... .......... .......... .......... .......... 8% 7.08M 13s
21300K .......... .......... .......... .......... .......... 8% 6.43M 13s
21350K .......... .......... .......... .......... .......... 8% 7.53M 13s
21400K .......... .......... .......... .......... .......... 8% 11.3M 13s
21450K .......... .......... .......... .......... .......... 8% 6.71M 13s
21500K .......... .......... .......... .......... .......... 8% 13.2M 13s
21550K .......... .......... .......... .......... .......... 8% 6.88M 13s
21600K .......... .......... .......... .......... .......... 8% 6.40M 13s
21650K .......... .......... .......... .......... .......... 8% 12.4M 13s
21700K .......... .......... .......... .......... .......... 8% 10.7M 13s
21750K .......... .......... .......... .......... .......... 8% 7.38M 13s
21800K .......... .......... .......... .......... .......... 8% 8.53M 13s
21850K .......... .......... .......... .......... .......... 8% 10.8M 13s
21900K .......... .......... .......... .......... .......... 8% 12.0M 13s
21950K .......... .......... .......... .......... .......... 8% 7.16M 13s
22000K .......... .......... .......... .......... .......... 8% 9.88M 13s
22050K .......... .......... .......... .......... .......... 8% 12.4M 13s
22100K .......... .......... .......... .......... .......... 8% 6.14M 13s
22150K .......... .......... .......... .......... .......... 8% 11.6M 13s
22200K .......... .......... .......... .......... .......... 8% 7.62M 13s
22250K .......... .......... .......... .......... .......... 8% 9.21M 13s
22300K .......... .......... .......... .......... .......... 8% 6.57M 13s
22350K .......... .......... .......... .......... .......... 8% 9.67M 13s
22400K .......... .......... .......... .......... .......... 8% 6.36M 13s
22450K .......... .......... .......... .......... .......... 8% 9.60M 13s
22500K .......... .......... .......... .......... .......... 8% 7.43M 14s
22550K .......... .......... .......... .......... .......... 8% 11.0M 14s
22600K .......... .......... .......... .......... .......... 8% 9.93M 14s
22650K .......... .......... .......... .......... .......... 8% 7.28M 14s
22700K .......... .......... .......... .......... .......... 8% 8.64M 14s
22750K .......... .......... .......... .......... .......... 8% 10.8M 14s
22800K .......... .......... .......... .......... .......... 8% 11.5M 14s
22850K .......... .......... .......... .......... .......... 8% 6.09M 14s
22900K .......... .......... .......... .......... .......... 8% 9.08M 14s
22950K .......... .......... .......... .......... .......... 8% 6.21M 14s
23000K .......... .......... .......... .......... .......... 8% 5.63M 14s
23050K .......... .......... .......... .......... .......... 8% 6.80M 14s
23100K .......... .......... .......... .......... .......... 8% 4.09M 14s
23150K .......... .......... .......... .......... .......... 8% 5.64M 14s
23200K .......... .......... .......... .......... .......... 8% 5.89M 14s
23250K .......... .......... .......... .......... .......... 8% 5.85M 14s
23300K .......... .......... .......... .......... .......... 8% 5.23M 14s
23350K .......... .......... .......... .......... .......... 8% 6.57M 14s
23400K .......... .......... .......... .......... .......... 8% 7.08M 14s
23450K .......... .......... .......... .......... .......... 8% 5.64M 14s
23500K .......... .......... .......... .......... .......... 8% 6.76M 14s
23550K .......... .......... .......... .......... .......... 8% 7.65M 14s
23600K .......... .......... .......... .......... .......... 8% 5.54M 14s
23650K .......... .......... .......... .......... .......... 8% 7.91M 14s
23700K .......... .......... .......... .......... .......... 8% 7.21M 15s
23750K .......... .......... .......... .......... .......... 8% 7.33M 15s
23800K .......... .......... .......... .......... .......... 8% 7.17M 15s
23850K .......... .......... .......... .......... .......... 9% 10.5M 15s
23900K .......... .......... .......... .......... .......... 9% 6.96M 15s
23950K .......... .......... .......... .......... .......... 9% 6.87M 15s
24000K .......... .......... .......... .......... .......... 9% 9.05M 15s
24050K .......... .......... .......... .......... .......... 9% 7.49M 15s
24100K .......... .......... .......... .......... .......... 9% 8.45M 15s
24150K .......... .......... .......... .......... .......... 9% 11.5M 15s
24200K .......... .......... .......... .......... .......... 9% 6.67M 15s
24250K .......... .......... .......... .......... .......... 9% 10.5M 15s
24300K .......... .......... .......... .......... .......... 9% 10.5M 15s
24350K .......... .......... .......... .......... .......... 9% 8.45M 15s
24400K .......... .......... .......... .......... .......... 9% 10.5M 15s
24450K .......... .......... .......... .......... .......... 9% 9.98M 15s
24500K .......... .......... .......... .......... .......... 9% 11.9M 15s
24550K .......... .......... .......... .......... .......... 9% 11.4M 15s
24600K .......... .......... .......... .......... .......... 9% 9.71M 15s
24650K .......... .......... .......... .......... .......... 9% 11.1M 15s
24700K .......... .......... .......... .......... .......... 9% 7.41M 15s
24750K .......... .......... .......... .......... .......... 9% 43.8M 15s
24800K .......... .......... .......... .......... .......... 9% 11.3M 15s
24850K .......... .......... .......... .......... .......... 9% 13.7M 15s
24900K .......... .......... .......... .......... .......... 9% 12.2M 15s
24950K .......... .......... .......... .......... .......... 9% 13.3M 15s
25000K .......... .......... .......... .......... .......... 9% 13.0M 15s
25050K .......... .......... .......... .......... .......... 9% 11.5M 15s
25100K .......... .......... .......... .......... .......... 9% 11.1M 15s
25150K .......... .......... .......... .......... .......... 9% 12.3M 15s
25200K .......... .......... .......... .......... .......... 9% 9.85M 15s
25250K .......... .......... .......... .......... .......... 9% 15.1M 15s
25300K .......... .......... .......... .......... .......... 9% 19.6M 15s
25350K .......... .......... .......... .......... .......... 9% 11.5M 15s
25400K .......... .......... .......... .......... .......... 9% 11.9M 15s
25450K .......... .......... .......... .......... .......... 9% 10.6M 15s
25500K .......... .......... .......... .......... .......... 9% 11.3M 15s
25550K .......... .......... .......... .......... .......... 9% 59.9M 15s
25600K .......... .......... .......... .......... .......... 9% 10.2M 15s
25650K .......... .......... .......... .......... .......... 9% 11.1M 15s
25700K .......... .......... .......... .......... .......... 9% 11.0M 15s
25750K .......... .......... .......... .......... .......... 9% 14.0M 15s
25800K .......... .......... .......... .......... .......... 9% 18.9M 15s
25850K .......... .......... .......... .......... .......... 9% 12.2M 15s
25900K .......... .......... .......... .......... .......... 9% 22.3M 15s
25950K .......... .......... .......... .......... .......... 9% 12.4M 15s
26000K .......... .......... .......... .......... .......... 9% 16.3M 15s
26050K .......... .......... .......... .......... .......... 9% 31.0M 15s
26100K .......... .......... .......... .......... .......... 9% 9.15M 15s
26150K .......... .......... .......... .......... .......... 9% 19.9M 15s
26200K .......... .......... .......... .......... .......... 9% 12.3M 15s
26250K .......... .......... .......... .......... .......... 9% 13.4M 15s
26300K .......... .......... .......... .......... .......... 9% 17.5M 15s
26350K .......... .......... .......... .......... .......... 9% 11.3M 15s
26400K .......... .......... .......... .......... .......... 9% 21.4M 15s
26450K .......... .......... .......... .......... .......... 9% 12.8M 15s
26500K .......... .......... .......... .......... .......... 9% 20.8M 15s
26550K .......... .......... .......... .......... .......... 10% 21.9M 15s
26600K .......... .......... .......... .......... .......... 10% 11.6M 15s
26650K .......... .......... .......... .......... .......... 10% 14.2M 15s
26700K .......... .......... .......... .......... .......... 10% 11.7M 15s
26750K .......... .......... .......... .......... .......... 10% 5.90M 15s
26800K .......... .......... .......... .......... .......... 10% 223M 15s
26850K .......... .......... .......... .......... .......... 10% 36.3M 15s
26900K .......... .......... .......... .......... .......... 10% 4.62M 15s
26950K .......... .......... .......... .......... .......... 10% 42.7M 15s
27000K .......... .......... .......... .......... .......... 10% 21.3M 15s
27050K .......... .......... .......... .......... .......... 10% 13.2M 15s
27100K .......... .......... .......... .......... .......... 10% 7.59M 15s
27150K .......... .......... .......... .......... .......... 10% 12.7M 15s
27200K .......... .......... .......... .......... .......... 10% 13.3M 15s
27250K .......... .......... .......... .......... .......... 10% 4.43M 15s
27300K .......... .......... .......... .......... .......... 10% 58.7M 15s
27350K .......... .......... .......... .......... .......... 10% 6.72M 15s
27400K .......... .......... .......... .......... .......... 10% 6.61M 15s
27450K .......... .......... .......... .......... .......... 10% 6.97M 15s
27500K .......... .......... .......... .......... .......... 10% 5.05M 15s
27550K .......... .......... .......... .......... .......... 10% 11.7M 15s
27600K .......... .......... .......... .......... .......... 10% 6.69M 15s
27650K .......... .......... .......... .......... .......... 10% 7.56M 15s
27700K .......... .......... .......... .......... .......... 10% 7.31M 15s
27750K .......... .......... .......... .......... .......... 10% 9.96M 15s
27800K .......... .......... .......... .......... .......... 10% 12.8M 15s
27850K .......... .......... .......... .......... .......... 10% 6.59M 15s
27900K .......... .......... .......... .......... .......... 10% 12.2M 15s
27950K .......... .......... .......... .......... .......... 10% 7.17M 15s
28000K .......... .......... .......... .......... .......... 10% 11.0M 15s
28050K .......... .......... .......... .......... .......... 10% 10.6M 15s
28100K .......... .......... .......... .......... .......... 10% 7.65M 15s
28150K .......... .......... .......... .......... .......... 10% 9.09M 15s
28200K .......... .......... .......... .......... .......... 10% 9.97M 15s
28250K .......... .......... .......... .......... .......... 10% 9.64M 15s
28300K .......... .......... .......... .......... .......... 10% 10.2M 15s
28350K .......... .......... .......... .......... .......... 10% 8.41M 15s
28400K .......... .......... .......... .......... .......... 10% 7.82M 16s
28450K .......... .......... .......... .......... .......... 10% 9.00M 16s
28500K .......... .......... .......... .......... .......... 10% 8.26M 16s
28550K .......... .......... .......... .......... .......... 10% 11.4M 16s
28600K .......... .......... .......... .......... .......... 10% 5.12M 16s
28650K .......... .......... .......... .......... .......... 10% 5.91M 16s
28700K .......... .......... .......... .......... .......... 10% 8.38M 16s
28750K .......... .......... .......... .......... .......... 10% 5.55M 16s
28800K .......... .......... .......... .......... .......... 10% 5.47M 16s
28850K .......... .......... .......... .......... .......... 10% 4.01M 16s
28900K .......... .......... .......... .......... .......... 10% 7.03M 16s
28950K .......... .......... .......... .......... .......... 10% 5.85M 16s
29000K .......... .......... .......... .......... .......... 10% 7.61M 16s
29050K .......... .......... .......... .......... .......... 10% 5.66M 16s
29100K .......... .......... .......... .......... .......... 10% 5.66M 16s
29150K .......... .......... .......... .......... .......... 10% 10.9M 16s
29200K .......... .......... .......... .......... .......... 11% 5.65M 16s
29250K .......... .......... .......... .......... .......... 11% 10.5M 16s
29300K .......... .......... .......... .......... .......... 11% 5.94M 16s
29350K .......... .......... .......... .......... .......... 11% 9.87M 16s
29400K .......... .......... .......... .......... .......... 11% 5.76M 16s
29450K .......... .......... .......... .......... .......... 11% 6.84M 16s
29500K .......... .......... .......... .......... .......... 11% 7.18M 16s
29550K .......... .......... .......... .......... .......... 11% 5.97M 16s
29600K .......... .......... .......... .......... .......... 11% 6.47M 16s
29650K .......... .......... .......... .......... .......... 11% 7.58M 16s
29700K .......... .......... .......... .......... .......... 11% 5.55M 16s
29750K .......... .......... .......... .......... .......... 11% 7.39M 16s
29800K .......... .......... .......... .......... .......... 11% 5.85M 16s
29850K .......... .......... .......... .......... .......... 11% 6.82M 16s
29900K .......... .......... .......... .......... .......... 11% 6.45M 16s
29950K .......... .......... .......... .......... .......... 11% 3.18M 16s
30000K .......... .......... .......... .......... .......... 11% 12.0M 16s
30050K .......... .......... .......... .......... .......... 11% 4.73M 17s
30100K .......... .......... .......... .......... .......... 11% 4.10M 17s
30150K .......... .......... .......... .......... .......... 11% 4.49M 17s
30200K .......... .......... .......... .......... .......... 11% 4.13M 17s
30250K .......... .......... .......... .......... .......... 11% 4.14M 17s
30300K .......... .......... .......... .......... .......... 11% 5.65M 17s
30350K .......... .......... .......... .......... .......... 11% 5.33M 17s
30400K .......... .......... .......... .......... .......... 11% 10.3M 17s
30450K .......... .......... .......... .......... .......... 11% 5.93M 17s
30500K .......... .......... .......... .......... .......... 11% 6.02M 17s
30550K .......... .......... .......... .......... .......... 11% 8.90M 17s
30600K .......... .......... .......... .......... .......... 11% 5.80M 17s
30650K .......... .......... .......... .......... .......... 11% 7.48M 17s
30700K .......... .......... .......... .......... .......... 11% 8.13M 17s
30750K .......... .......... .......... .......... .......... 11% 6.53M 17s
30800K .......... .......... .......... .......... .......... 11% 9.23M 17s
30850K .......... .......... .......... .......... .......... 11% 8.30M 17s
30900K .......... .......... .......... .......... .......... 11% 7.50M 17s
30950K .......... .......... .......... .......... .......... 11% 8.34M 17s
31000K .......... .......... .......... .......... .......... 11% 10.7M 17s
31050K .......... .......... .......... .......... .......... 11% 8.46M 17s
31100K .......... .......... .......... .......... .......... 11% 8.05M 17s
31150K .......... .......... .......... .......... .......... 11% 10.7M 17s
31200K .......... .......... .......... .......... .......... 11% 9.66M 17s
31250K .......... .......... .......... .......... .......... 11% 13.4M 17s
31300K .......... .......... .......... .......... .......... 11% 8.70M 17s
31350K .......... .......... .......... .......... .......... 11% 10.7M 17s
31400K .......... .......... .......... .......... .......... 11% 12.8M 17s
31450K .......... .......... .......... .......... .......... 11% 9.75M 17s
31500K .......... .......... .......... .......... .......... 11% 15.3M 17s
31550K .......... .......... .......... .......... .......... 11% 12.4M 17s
31600K .......... .......... .......... .......... .......... 11% 10.0M 17s
31650K .......... .......... .......... .......... .......... 11% 13.7M 17s
31700K .......... .......... .......... .......... .......... 11% 11.4M 17s
31750K .......... .......... .......... .......... .......... 11% 13.6M 17s
31800K .......... .......... .......... .......... .......... 11% 11.2M 17s
31850K .......... .......... .......... .......... .......... 12% 13.6M 17s
31900K .......... .......... .......... .......... .......... 12% 19.3M 17s
31950K .......... .......... .......... .......... .......... 12% 15.2M 17s
32000K .......... .......... .......... .......... .......... 12% 14.9M 17s
32050K .......... .......... .......... .......... .......... 12% 13.4M 17s
32100K .......... .......... .......... .......... .......... 12% 13.4M 17s
32150K .......... .......... .......... .......... .......... 12% 16.4M 17s
32200K .......... .......... .......... .......... .......... 12% 9.55M 17s
32250K .......... .......... .......... .......... .......... 12% 11.4M 17s
32300K .......... .......... .......... .......... .......... 12% 27.6M 17s
32350K .......... .......... .......... .......... .......... 12% 14.0M 17s
32400K .......... .......... .......... .......... .......... 12% 14.6M 17s
32450K .......... .......... .......... .......... .......... 12% 13.8M 17s
32500K .......... .......... .......... .......... .......... 12% 14.7M 17s
32550K .......... .......... .......... .......... .......... 12% 14.3M 17s
32600K .......... .......... .......... .......... .......... 12% 12.4M 17s
32650K .......... .......... .......... .......... .......... 12% 14.7M 17s
32700K .......... .......... .......... .......... .......... 12% 7.46M 17s
32750K .......... .......... .......... .......... .......... 12% 34.3M 17s
32800K .......... .......... .......... .......... .......... 12% 11.6M 17s
32850K .......... .......... .......... .......... .......... 12% 12.8M 17s
32900K .......... .......... .......... .......... .......... 12% 12.6M 17s
32950K .......... .......... .......... .......... .......... 12% 10.5M 17s
33000K .......... .......... .......... .......... .......... 12% 8.34M 17s
33050K .......... .......... .......... .......... .......... 12% 17.8M 17s
33100K .......... .......... .......... .......... .......... 12% 9.11M 17s
33150K .......... .......... .......... .......... .......... 12% 12.2M 17s
33200K .......... .......... .......... .......... .......... 12% 12.2M 17s
33250K .......... .......... .......... .......... .......... 12% 12.1M 17s
33300K .......... .......... .......... .......... .......... 12% 6.52M 17s
33350K .......... .......... .......... .......... .......... 12% 44.3M 17s
33400K .......... .......... .......... .......... .......... 12% 10.2M 17s
33450K .......... .......... .......... .......... .......... 12% 16.2M 17s
33500K .......... .......... .......... .......... .......... 12% 10.2M 17s
33550K .......... .......... .......... .......... .......... 12% 10.8M 17s
33600K .......... .......... .......... .......... .......... 12% 10.6M 17s
33650K .......... .......... .......... .......... .......... 12% 10.6M 17s
33700K .......... .......... .......... .......... .......... 12% 8.71M 17s
33750K .......... .......... .......... .......... .......... 12% 13.9M 17s
33800K .......... .......... .......... .......... .......... 12% 14.1M 17s
33850K .......... .......... .......... .......... .......... 12% 8.98M 17s
33900K .......... .......... .......... .......... .......... 12% 15.1M 17s
33950K .......... .......... .......... .......... .......... 12% 13.6M 17s
34000K .......... .......... .......... .......... .......... 12% 15.1M 17s
34050K .......... .......... .......... .......... .......... 12% 16.7M 17s
34100K .......... .......... .......... .......... .......... 12% 7.38M 17s
34150K .......... .......... .......... .......... .......... 12% 17.2M 17s
34200K .......... .......... .......... .......... .......... 12% 13.1M 17s
34250K .......... .......... .......... .......... .......... 12% 16.6M 17s
34300K .......... .......... .......... .......... .......... 12% 15.5M 17s
34350K .......... .......... .......... .......... .......... 12% 12.4M 17s
34400K .......... .......... .......... .......... .......... 12% 14.2M 17s
34450K .......... .......... .......... .......... .......... 12% 14.1M 17s
34500K .......... .......... .......... .......... .......... 13% 12.5M 17s
34550K .......... .......... .......... .......... .......... 13% 15.1M 17s
34600K .......... .......... .......... .......... .......... 13% 13.3M 17s
34650K .......... .......... .......... .......... .......... 13% 11.6M 17s
34700K .......... .......... .......... .......... .......... 13% 13.2M 17s
34750K .......... .......... .......... .......... .......... 13% 13.6M 17s
34800K .......... .......... .......... .......... .......... 13% 14.3M 17s
34850K .......... .......... .......... .......... .......... 13% 10.9M 17s
34900K .......... .......... .......... .......... .......... 13% 11.6M 17s
34950K .......... .......... .......... .......... .......... 13% 12.8M 17s
35000K .......... .......... .......... .......... .......... 13% 12.8M 17s
35050K .......... .......... .......... .......... .......... 13% 7.72M 17s
35100K .......... .......... .......... .......... .......... 13% 56.3M 17s
35150K .......... .......... .......... .......... .......... 13% 12.9M 17s
35200K .......... .......... .......... .......... .......... 13% 7.84M 17s
35250K .......... .......... .......... .......... .......... 13% 9.13M 17s
35300K .......... .......... .......... .......... .......... 13% 12.7M 17s
35350K .......... .......... .......... .......... .......... 13% 10.6M 17s
35400K .......... .......... .......... .......... .......... 13% 12.2M 17s
35450K .......... .......... .......... .......... .......... 13% 6.08M 17s
35500K .......... .......... .......... .......... .......... 13% 12.4M 17s
35550K .......... .......... .......... .......... .......... 13% 12.0M 17s
35600K .......... .......... .......... .......... .......... 13% 9.76M 17s
35650K .......... .......... .......... .......... .......... 13% 12.9M 17s
35700K .......... .......... .......... .......... .......... 13% 11.1M 17s
35750K .......... .......... .......... .......... .......... 13% 7.30M 17s
35800K .......... .......... .......... .......... .......... 13% 15.0M 17s
35850K .......... .......... .......... .......... .......... 13% 8.84M 17s
35900K .......... .......... .......... .......... .......... 13% 14.9M 17s
35950K .......... .......... .......... .......... .......... 13% 9.40M 17s
36000K .......... .......... .......... .......... .......... 13% 22.6M 17s
36050K .......... .......... .......... .......... .......... 13% 12.7M 17s
36100K .......... .......... .......... .......... .......... 13% 11.4M 17s
36150K .......... .......... .......... .......... .......... 13% 22.4M 17s
36200K .......... .......... .......... .......... .......... 13% 8.64M 17s
36250K .......... .......... .......... .......... .......... 13% 21.4M 17s
36300K .......... .......... .......... .......... .......... 13% 10.6M 17s
36350K .......... .......... .......... .......... .......... 13% 10.9M 17s
36400K .......... .......... .......... .......... .......... 13% 13.1M 17s
36450K .......... .......... .......... .......... .......... 13% 10.3M 17s
36500K .......... .......... .......... .......... .......... 13% 16.3M 17s
36550K .......... .......... .......... .......... .......... 13% 14.7M 17s
36600K .......... .......... .......... .......... .......... 13% 11.3M 17s
36650K .......... .......... .......... .......... .......... 13% 13.1M 17s
36700K .......... .......... .......... .......... .......... 13% 9.82M 17s
36750K .......... .......... .......... .......... .......... 13% 14.3M 17s
36800K .......... .......... .......... .......... .......... 13% 13.4M 17s
36850K .......... .......... .......... .......... .......... 13% 5.72M 17s
36900K .......... .......... .......... .......... .......... 13% 23.7M 17s
36950K .......... .......... .......... .......... .......... 13% 26.2M 17s
37000K .......... .......... .......... .......... .......... 13% 9.65M 17s
37050K .......... .......... .......... .......... .......... 13% 9.00M 17s
37100K .......... .......... .......... .......... .......... 13% 8.97M 17s
37150K .......... .......... .......... .......... .......... 14% 10.9M 17s
37200K .......... .......... .......... .......... .......... 14% 9.02M 17s
37250K .......... .......... .......... .......... .......... 14% 9.31M 17s
37300K .......... .......... .......... .......... .......... 14% 13.2M 17s
37350K .......... .......... .......... .......... .......... 14% 8.72M 17s
37400K .......... .......... .......... .......... .......... 14% 11.3M 17s
37450K .......... .......... .......... .......... .......... 14% 8.26M 17s
37500K .......... .......... .......... .......... .......... 14% 11.2M 17s
37550K .......... .......... .......... .......... .......... 14% 12.3M 17s
37600K .......... .......... .......... .......... .......... 14% 10.8M 17s
37650K .......... .......... .......... .......... .......... 14% 11.5M 17s
37700K .......... .......... .......... .......... .......... 14% 7.99M 17s
37750K .......... .......... .......... .......... .......... 14% 13.5M 17s
37800K .......... .......... .......... .......... .......... 14% 10.0M 17s
37850K .......... .......... .......... .......... .......... 14% 12.6M 17s
37900K .......... .......... .......... .......... .......... 14% 18.8M 17s
37950K .......... .......... .......... .......... .......... 14% 7.62M 17s
38000K .......... .......... .......... .......... .......... 14% 13.2M 17s
38050K .......... .......... .......... .......... .......... 14% 25.5M 17s
38100K .......... .......... .......... .......... .......... 14% 11.3M 17s
38150K .......... .......... .......... .......... .......... 14% 12.5M 17s
38200K .......... .......... .......... .......... .......... 14% 12.0M 17s
38250K .......... .......... .......... .......... .......... 14% 12.8M 17s
38300K .......... .......... .......... .......... .......... 14% 12.2M 17s
38350K .......... .......... .......... .......... .......... 14% 11.4M 17s
38400K .......... .......... .......... .......... .......... 14% 12.7M 17s
38450K .......... .......... .......... .......... .......... 14% 11.4M 17s
38500K .......... .......... .......... .......... .......... 14% 11.8M 17s
38550K .......... .......... .......... .......... .......... 14% 11.0M 17s
38600K .......... .......... .......... .......... .......... 14% 11.6M 17s
38650K .......... .......... .......... .......... .......... 14% 25.7M 17s
38700K .......... .......... .......... .......... .......... 14% 9.94M 17s
38750K .......... .......... .......... .......... .......... 14% 11.2M 17s
38800K .......... .......... .......... .......... .......... 14% 15.8M 17s
38850K .......... .......... .......... .......... .......... 14% 16.8M 17s
38900K .......... .......... .......... .......... .......... 14% 20.3M 17s
38950K .......... .......... .......... .......... .......... 14% 13.0M 17s
39000K .......... .......... .......... .......... .......... 14% 10.5M 17s
39050K .......... .......... .......... .......... .......... 14% 11.3M 17s
39100K .......... .......... .......... .......... .......... 14% 15.5M 17s
39150K .......... .......... .......... .......... .......... 14% 36.2M 17s
39200K .......... .......... .......... .......... .......... 14% 12.9M 17s
39250K .......... .......... .......... .......... .......... 14% 15.3M 17s
39300K .......... .......... .......... .......... .......... 14% 23.0M 17s
39350K .......... .......... .......... .......... .......... 14% 19.3M 17s
39400K .......... .......... .......... .......... .......... 14% 11.0M 17s
39450K .......... .......... .......... .......... .......... 14% 19.7M 17s
39500K .......... .......... .......... .......... .......... 14% 16.8M 17s
39550K .......... .......... .......... .......... .......... 14% 12.4M 17s
39600K .......... .......... .......... .......... .......... 14% 17.3M 17s
39650K .......... .......... .......... .......... .......... 14% 14.7M 17s
39700K .......... .......... .......... .......... .......... 14% 14.4M 17s
39750K .......... .......... .......... .......... .......... 14% 12.8M 17s
39800K .......... .......... .......... .......... .......... 15% 22.2M 17s
39850K .......... .......... .......... .......... .......... 15% 11.4M 17s
39900K .......... .......... .......... .......... .......... 15% 17.1M 17s
39950K .......... .......... .......... .......... .......... 15% 10.9M 17s
40000K .......... .......... .......... .......... .......... 15% 18.5M 17s
40050K .......... .......... .......... .......... .......... 15% 11.8M 17s
40100K .......... .......... .......... .......... .......... 15% 14.1M 17s
40150K .......... .......... .......... .......... .......... 15% 16.9M 17s
40200K .......... .......... .......... .......... .......... 15% 11.4M 17s
40250K .......... .......... .......... .......... .......... 15% 18.1M 17s
40300K .......... .......... .......... .......... .......... 15% 21.7M 17s
40350K .......... .......... .......... .......... .......... 15% 11.0M 17s
40400K .......... .......... .......... .......... .......... 15% 16.7M 17s
40450K .......... .......... .......... .......... .......... 15% 21.2M 17s
40500K .......... .......... .......... .......... .......... 15% 15.3M 17s
40550K .......... .......... .......... .......... .......... 15% 15.3M 17s
40600K .......... .......... .......... .......... .......... 15% 20.2M 17s
40650K .......... .......... .......... .......... .......... 15% 6.15M 17s
40700K .......... .......... .......... .......... .......... 15% 52.7M 17s
40750K .......... .......... .......... .......... .......... 15% 79.3M 17s
40800K .......... .......... .......... .......... .......... 15% 8.08M 17s
40850K .......... .......... .......... .......... .......... 15% 10.1M 17s
40900K .......... .......... .......... .......... .......... 15% 11.5M 17s
40950K .......... .......... .......... .......... .......... 15% 8.81M 17s
41000K .......... .......... .......... .......... .......... 15% 8.64M 17s
41050K .......... .......... .......... .......... .......... 15% 9.32M 17s
41100K .......... .......... .......... .......... .......... 15% 8.17M 17s
41150K .......... .......... .......... .......... .......... 15% 9.54M 17s
41200K .......... .......... .......... .......... .......... 15% 7.02M 17s
41250K .......... .......... .......... .......... .......... 15% 11.2M 17s
41300K .......... .......... .......... .......... .......... 15% 7.42M 17s
41350K .......... .......... .......... .......... .......... 15% 8.08M 17s
41400K .......... .......... .......... .......... .......... 15% 9.78M 17s
41450K .......... .......... .......... .......... .......... 15% 6.62M 17s
41500K .......... .......... .......... .......... .......... 15% 5.75M 17s
41550K .......... .......... .......... .......... .......... 15% 8.73M 17s
41600K .......... .......... .......... .......... .......... 15% 6.47M 17s
41650K .......... .......... .......... .......... .......... 15% 9.47M 17s
41700K .......... .......... .......... .......... .......... 15% 5.43M 17s
41750K .......... .......... .......... .......... .......... 15% 8.72M 17s
41800K .......... .......... .......... .......... .......... 15% 5.36M 17s
41850K .......... .......... .......... .......... .......... 15% 9.01M 17s
41900K .......... .......... .......... .......... .......... 15% 8.34M 17s
41950K .......... .......... .......... .......... .......... 15% 6.30M 17s
42000K .......... .......... .......... .......... .......... 15% 9.37M 17s
42050K .......... .......... .......... .......... .......... 15% 7.86M 17s
42100K .......... .......... .......... .......... .......... 15% 6.40M 17s
42150K .......... .......... .......... .......... .......... 15% 10.3M 17s
42200K .......... .......... .......... .......... .......... 15% 6.89M 17s
42250K .......... .......... .......... .......... .......... 15% 9.55M 17s
42300K .......... .......... .......... .......... .......... 15% 4.06M 17s
42350K .......... .......... .......... .......... .......... 15% 6.76M 17s
42400K .......... .......... .......... .......... .......... 15% 4.83M 17s
42450K .......... .......... .......... .......... .......... 16% 3.37M 17s
42500K .......... .......... .......... .......... .......... 16% 5.27M 17s
42550K .......... .......... .......... .......... .......... 16% 5.68M 17s
42600K .......... .......... .......... .......... .......... 16% 5.05M 17s
42650K .......... .......... .......... .......... .......... 16% 6.51M 17s
42700K .......... .......... .......... .......... .......... 16% 5.60M 17s
42750K .......... .......... .......... .......... .......... 16% 9.36M 17s
42800K .......... .......... .......... .......... .......... 16% 7.88M 17s
42850K .......... .......... .......... .......... .......... 16% 6.80M 17s
42900K .......... .......... .......... .......... .......... 16% 8.04M 17s
42950K .......... .......... .......... .......... .......... 16% 6.19M 17s
43000K .......... .......... .......... .......... .......... 16% 10.9M 17s
43050K .......... .......... .......... .......... .......... 16% 7.60M 17s
43100K .......... .......... .......... .......... .......... 16% 8.61M 17s
43150K .......... .......... .......... .......... .......... 16% 8.01M 17s
43200K .......... .......... .......... .......... .......... 16% 8.09M 17s
43250K .......... .......... .......... .......... .......... 16% 9.10M 17s
43300K .......... .......... .......... .......... .......... 16% 7.83M 17s
43350K .......... .......... .......... .......... .......... 16% 6.68M 17s
43400K .......... .......... .......... .......... .......... 16% 9.90M 17s
43450K .......... .......... .......... .......... .......... 16% 6.84M 17s
43500K .......... .......... .......... .......... .......... 16% 7.58M 17s
43550K .......... .......... .......... .......... .......... 16% 11.7M 17s
43600K .......... .......... .......... .......... .......... 16% 6.70M 17s
43650K .......... .......... .......... .......... .......... 16% 13.7M 17s
43700K .......... .......... .......... .......... .......... 16% 8.99M 17s
43750K .......... .......... .......... .......... .......... 16% 12.3M 17s
43800K .......... .......... .......... .......... .......... 16% 10.0M 17s
43850K .......... .......... .......... .......... .......... 16% 10.9M 17s
43900K .......... .......... .......... .......... .......... 16% 12.0M 17s
43950K .......... .......... .......... .......... .......... 16% 9.05M 17s
44000K .......... .......... .......... .......... .......... 16% 13.1M 17s
44050K .......... .......... .......... .......... .......... 16% 11.4M 17s
44100K .......... .......... .......... .......... .......... 16% 10.1M 17s
44150K .......... .......... .......... .......... .......... 16% 12.6M 17s
44200K .......... .......... .......... .......... .......... 16% 10.7M 17s
44250K .......... .......... .......... .......... .......... 16% 11.7M 17s
44300K .......... .......... .......... .......... .......... 16% 11.3M 17s
44350K .......... .......... .......... .......... .......... 16% 7.07M 17s
44400K .......... .......... .......... .......... .......... 16% 23.7M 17s
44450K .......... .......... .......... .......... .......... 16% 11.2M 17s
44500K .......... .......... .......... .......... .......... 16% 10.7M 17s
44550K .......... .......... .......... .......... .......... 16% 13.0M 17s
44600K .......... .......... .......... .......... .......... 16% 10.1M 17s
44650K .......... .......... .......... .......... .......... 16% 12.2M 17s
44700K .......... .......... .......... .......... .......... 16% 11.5M 17s
44750K .......... .......... .......... .......... .......... 16% 13.7M 17s
44800K .......... .......... .......... .......... .......... 16% 17.3M 17s
44850K .......... .......... .......... .......... .......... 16% 4.67M 17s
44900K .......... .......... .......... .......... .......... 16% 36.2M 17s
44950K .......... .......... .......... .......... .......... 16% 44.8M 17s
45000K .......... .......... .......... .......... .......... 16% 7.88M 17s
45050K .......... .......... .......... .......... .......... 16% 11.3M 17s
45100K .......... .......... .......... .......... .......... 17% 9.15M 17s
45150K .......... .......... .......... .......... .......... 17% 11.5M 17s
45200K .......... .......... .......... .......... .......... 17% 11.0M 17s
45250K .......... .......... .......... .......... .......... 17% 12.2M 17s
45300K .......... .......... .......... .......... .......... 17% 6.13M 17s
45350K .......... .......... .......... .......... .......... 17% 9.04M 17s
45400K .......... .......... .......... .......... .......... 17% 11.7M 17s
45450K .......... .......... .......... .......... .......... 17% 10.6M 17s
45500K .......... .......... .......... .......... .......... 17% 10.6M 17s
45550K .......... .......... .......... .......... .......... 17% 5.33M 17s
45600K .......... .......... .......... .......... .......... 17% 66.2M 17s
45650K .......... .......... .......... .......... .......... 17% 10.6M 17s
45700K .......... .......... .......... .......... .......... 17% 6.13M 17s
45750K .......... .......... .......... .......... .......... 17% 5.83M 17s
45800K .......... .......... .......... .......... .......... 17% 7.11M 17s
45850K .......... .......... .......... .......... .......... 17% 5.97M 17s
45900K .......... .......... .......... .......... .......... 17% 9.24M 17s
45950K .......... .......... .......... .......... .......... 17% 4.05M 17s
46000K .......... .......... .......... .......... .......... 17% 9.14M 17s
46050K .......... .......... .......... .......... .......... 17% 5.78M 17s
46100K .......... .......... .......... .......... .......... 17% 5.80M 17s
46150K .......... .......... .......... .......... .......... 17% 11.6M 17s
46200K .......... .......... .......... .......... .......... 17% 5.91M 17s
46250K .......... .......... .......... .......... .......... 17% 7.05M 17s
46300K .......... .......... .......... .......... .......... 17% 9.23M 17s
46350K .......... .......... .......... .......... .......... 17% 11.0M 17s
46400K .......... .......... .......... .......... .......... 17% 5.29M 17s
46450K .......... .......... .......... .......... .......... 17% 12.1M 17s
46500K .......... .......... .......... .......... .......... 17% 9.36M 17s
46550K .......... .......... .......... .......... .......... 17% 8.53M 17s
46600K .......... .......... .......... .......... .......... 17% 8.01M 17s
46650K .......... .......... .......... .......... .......... 17% 9.82M 17s
46700K .......... .......... .......... .......... .......... 17% 10.3M 17s
46750K .......... .......... .......... .......... .......... 17% 12.2M 17s
46800K .......... .......... .......... .......... .......... 17% 7.08M 18s
46850K .......... .......... .......... .......... .......... 17% 8.21M 18s
46900K .......... .......... .......... .......... .......... 17% 10.3M 18s
46950K .......... .......... .......... .......... .......... 17% 9.54M 18s
47000K .......... .......... .......... .......... .......... 17% 8.91M 18s
47050K .......... .......... .......... .......... .......... 17% 11.3M 18s
47100K .......... .......... .......... .......... .......... 17% 8.71M 18s
47150K .......... .......... .......... .......... .......... 17% 11.8M 18s
47200K .......... .......... .......... .......... .......... 17% 11.1M 18s
47250K .......... .......... .......... .......... .......... 17% 12.9M 17s
47300K .......... .......... .......... .......... .......... 17% 11.2M 17s
47350K .......... .......... .......... .......... .......... 17% 8.72M 18s
47400K .......... .......... .......... .......... .......... 17% 11.1M 17s
47450K .......... .......... .......... .......... .......... 17% 11.1M 17s
47500K .......... .......... .......... .......... .......... 17% 11.0M 17s
47550K .......... .......... .......... .......... .......... 17% 11.7M 17s
47600K .......... .......... .......... .......... .......... 17% 11.2M 17s
47650K .......... .......... .......... .......... .......... 17% 13.2M 17s
47700K .......... .......... .......... .......... .......... 17% 8.12M 17s
47750K .......... .......... .......... .......... .......... 18% 12.6M 17s
47800K .......... .......... .......... .......... .......... 18% 26.0M 17s
47850K .......... .......... .......... .......... .......... 18% 12.3M 17s
47900K .......... .......... .......... .......... .......... 18% 15.3M 17s
47950K .......... .......... .......... .......... .......... 18% 13.0M 17s
48000K .......... .......... .......... .......... .......... 18% 12.0M 17s
48050K .......... .......... .......... .......... .......... 18% 13.3M 17s
48100K .......... .......... .......... .......... .......... 18% 10.1M 17s
48150K .......... .......... .......... .......... .......... 18% 16.1M 17s
48200K .......... .......... .......... .......... .......... 18% 12.9M 17s
48250K .......... .......... .......... .......... .......... 18% 23.2M 17s
48300K .......... .......... .......... .......... .......... 18% 12.2M 17s
48350K .......... .......... .......... .......... .......... 18% 12.5M 17s
48400K .......... .......... .......... .......... .......... 18% 13.3M 17s
48450K .......... .......... .......... .......... .......... 18% 13.7M 17s
48500K .......... .......... .......... .......... .......... 18% 24.1M 17s
48550K .......... .......... .......... .......... .......... 18% 14.1M 17s
48600K .......... .......... .......... .......... .......... 18% 10.1M 17s
48650K .......... .......... .......... .......... .......... 18% 18.2M 17s
48700K .......... .......... .......... .......... .......... 18% 12.8M 17s
48750K .......... .......... .......... .......... .......... 18% 43.5M 17s
48800K .......... .......... .......... .......... .......... 18% 11.5M 17s
48850K .......... .......... .......... .......... .......... 18% 13.6M 17s
48900K .......... .......... .......... .......... .......... 18% 33.4M 17s
48950K .......... .......... .......... .......... .......... 18% 11.3M 17s
49000K .......... .......... .......... .......... .......... 18% 16.5M 17s
49050K .......... .......... .......... .......... .......... 18% 13.8M 17s
49100K .......... .......... .......... .......... .......... 18% 13.0M 17s
49150K .......... .......... .......... .......... .......... 18% 26.9M 17s
49200K .......... .......... .......... .......... .......... 18% 12.5M 17s
49250K .......... .......... .......... .......... .......... 18% 12.9M 17s
49300K .......... .......... .......... .......... .......... 18% 26.3M 17s
49350K .......... .......... .......... .......... .......... 18% 12.6M 17s
49400K .......... .......... .......... .......... .......... 18% 11.7M 17s
49450K .......... .......... .......... .......... .......... 18% 48.2M 17s
49500K .......... .......... .......... .......... .......... 18% 11.4M 17s
49550K .......... .......... .......... .......... .......... 18% 12.2M 17s
49600K .......... .......... .......... .......... .......... 18% 14.5M 17s
49650K .......... .......... .......... .......... .......... 18% 16.8M 17s
49700K .......... .......... .......... .......... .......... 18% 6.02M 17s
49750K .......... .......... .......... .......... .......... 18% 186M 17s
49800K .......... .......... .......... .......... .......... 18% 20.4M 17s
49850K .......... .......... .......... .......... .......... 18% 10.7M 17s
49900K .......... .......... .......... .......... .......... 18% 13.5M 17s
49950K .......... .......... .......... .......... .......... 18% 10.3M 17s
50000K .......... .......... .......... .......... .......... 18% 11.6M 17s
50050K .......... .......... .......... .......... .......... 18% 11.7M 17s
50100K .......... .......... .......... .......... .......... 18% 10.5M 17s
50150K .......... .......... .......... .......... .......... 18% 5.99M 17s
50200K .......... .......... .......... .......... .......... 18% 47.1M 17s
50250K .......... .......... .......... .......... .......... 18% 10.8M 17s
50300K .......... .......... .......... .......... .......... 18% 10.0M 17s
50350K .......... .......... .......... .......... .......... 18% 8.03M 17s
50400K .......... .......... .......... .......... .......... 19% 10.1M 17s
50450K .......... .......... .......... .......... .......... 19% 7.73M 17s
50500K .......... .......... .......... .......... .......... 19% 11.8M 17s
50550K .......... .......... .......... .......... .......... 19% 12.2M 17s
50600K .......... .......... .......... .......... .......... 19% 6.56M 17s
50650K .......... .......... .......... .......... .......... 19% 15.1M 17s
50700K .......... .......... .......... .......... .......... 19% 6.40M 17s
50750K .......... .......... .......... .......... .......... 19% 13.1M 17s
50800K .......... .......... .......... .......... .......... 19% 11.7M 17s
50850K .......... .......... .......... .......... .......... 19% 11.1M 17s
50900K .......... .......... .......... .......... .......... 19% 9.96M 17s
50950K .......... .......... .......... .......... .......... 19% 9.82M 17s
51000K .......... .......... .......... .......... .......... 19% 11.1M 17s
51050K .......... .......... .......... .......... .......... 19% 13.2M 17s
51100K .......... .......... .......... .......... .......... 19% 11.1M 17s
51150K .......... .......... .......... .......... .......... 19% 13.7M 17s
51200K .......... .......... .......... .......... .......... 19% 12.4M 17s
51250K .......... .......... .......... .......... .......... 19% 13.8M 17s
51300K .......... .......... .......... .......... .......... 19% 13.2M 17s
51350K .......... .......... .......... .......... .......... 19% 10.3M 17s
51400K .......... .......... .......... .......... .......... 19% 13.0M 17s
51450K .......... .......... .......... .......... .......... 19% 16.0M 17s
51500K .......... .......... .......... .......... .......... 19% 11.9M 17s
51550K .......... .......... .......... .......... .......... 19% 12.2M 17s
51600K .......... .......... .......... .......... .......... 19% 8.40M 17s
51650K .......... .......... .......... .......... .......... 19% 21.8M 17s
51700K .......... .......... .......... .......... .......... 19% 11.7M 17s
51750K .......... .......... .......... .......... .......... 19% 12.5M 17s
51800K .......... .......... .......... .......... .......... 19% 11.7M 17s
51850K .......... .......... .......... .......... .......... 19% 11.1M 17s
51900K .......... .......... .......... .......... .......... 19% 5.41M 17s
51950K .......... .......... .......... .......... .......... 19% 116M 17s
52000K .......... .......... .......... .......... .......... 19% 10.5M 17s
52050K .......... .......... .......... .......... .......... 19% 11.6M 17s
52100K .......... .......... .......... .......... .......... 19% 8.62M 17s
52150K .......... .......... .......... .......... .......... 19% 11.8M 17s
52200K .......... .......... .......... .......... .......... 19% 11.0M 17s
52250K .......... .......... .......... .......... .......... 19% 8.50M 17s
52300K .......... .......... .......... .......... .......... 19% 13.2M 17s
52350K .......... .......... .......... .......... .......... 19% 11.8M 17s
52400K .......... .......... .......... .......... .......... 19% 11.7M 17s
52450K .......... .......... .......... .......... .......... 19% 13.9M 17s
52500K .......... .......... .......... .......... .......... 19% 10.4M 17s
52550K .......... .......... .......... .......... .......... 19% 11.0M 17s
52600K .......... .......... .......... .......... .......... 19% 7.78M 17s
52650K .......... .......... .......... .......... .......... 19% 9.96M 17s
52700K .......... .......... .......... .......... .......... 19% 11.5M 17s
52750K .......... .......... .......... .......... .......... 19% 10.9M 17s
52800K .......... .......... .......... .......... .......... 19% 10.5M 17s
52850K .......... .......... .......... .......... .......... 19% 8.03M 17s
52900K .......... .......... .......... .......... .......... 19% 7.42M 17s
52950K .......... .......... .......... .......... .......... 19% 10.6M 17s
53000K .......... .......... .......... .......... .......... 19% 22.0M 17s
53050K .......... .......... .......... .......... .......... 19% 11.5M 17s
53100K .......... .......... .......... .......... .......... 20% 16.4M 17s
53150K .......... .......... .......... .......... .......... 20% 7.33M 17s
53200K .......... .......... .......... .......... .......... 20% 10.7M 17s
53250K .......... .......... .......... .......... .......... 20% 10.1M 17s
53300K .......... .......... .......... .......... .......... 20% 10.4M 17s
53350K .......... .......... .......... .......... .......... 20% 9.58M 17s
53400K .......... .......... .......... .......... .......... 20% 9.40M 17s
53450K .......... .......... .......... .......... .......... 20% 11.4M 17s
53500K .......... .......... .......... .......... .......... 20% 15.4M 17s
53550K .......... .......... .......... .......... .......... 20% 10.9M 17s
53600K .......... .......... .......... .......... .......... 20% 9.06M 17s
53650K .......... .......... .......... .......... .......... 20% 8.97M 17s
53700K .......... .......... .......... .......... .......... 20% 14.2M 17s
53750K .......... .......... .......... .......... .......... 20% 13.5M 17s
53800K .......... .......... .......... .......... .......... 20% 18.1M 17s
53850K .......... .......... .......... .......... .......... 20% 12.1M 17s
53900K .......... .......... .......... .......... .......... 20% 13.0M 17s
53950K .......... .......... .......... .......... .......... 20% 14.1M 17s
54000K .......... .......... .......... .......... .......... 20% 17.2M 17s
54050K .......... .......... .......... .......... .......... 20% 15.0M 17s
54100K .......... .......... .......... .......... .......... 20% 6.04M 17s
54150K .......... .......... .......... .......... .......... 20% 83.1M 17s
54200K .......... .......... .......... .......... .......... 20% 17.4M 17s
54250K .......... .......... .......... .......... .......... 20% 9.75M 17s
54300K .......... .......... .......... .......... .......... 20% 10.6M 17s
54350K .......... .......... .......... .......... .......... 20% 8.06M 17s
54400K .......... .......... .......... .......... .......... 20% 11.9M 17s
54450K .......... .......... .......... .......... .......... 20% 7.68M 17s
54500K .......... .......... .......... .......... .......... 20% 8.78M 17s
54550K .......... .......... .......... .......... .......... 20% 11.2M 17s
54600K .......... .......... .......... .......... .......... 20% 9.26M 17s
54650K .......... .......... .......... .......... .......... 20% 11.9M 17s
54700K .......... .......... .......... .......... .......... 20% 8.33M 17s
54750K .......... .......... .......... .......... .......... 20% 15.0M 17s
54800K .......... .......... .......... .......... .......... 20% 10.8M 17s
54850K .......... .......... .......... .......... .......... 20% 8.77M 17s
54900K .......... .......... .......... .......... .......... 20% 9.96M 17s
54950K .......... .......... .......... .......... .......... 20% 9.98M 17s
55000K .......... .......... .......... .......... .......... 20% 11.3M 17s
55050K .......... .......... .......... .......... .......... 20% 11.6M 17s
55100K .......... .......... .......... .......... .......... 20% 12.5M 17s
55150K .......... .......... .......... .......... .......... 20% 11.1M 17s
55200K .......... .......... .......... .......... .......... 20% 8.34M 17s
55250K .......... .......... .......... .......... .......... 20% 18.9M 17s
55300K .......... .......... .......... .......... .......... 20% 10.6M 17s
55350K .......... .......... .......... .......... .......... 20% 13.0M 17s
55400K .......... .......... .......... .......... .......... 20% 12.0M 17s
55450K .......... .......... .......... .......... .......... 20% 11.2M 17s
55500K .......... .......... .......... .......... .......... 20% 13.0M 17s
55550K .......... .......... .......... .......... .......... 20% 13.4M 17s
55600K .......... .......... .......... .......... .......... 20% 11.4M 17s
55650K .......... .......... .......... .......... .......... 20% 10.9M 17s
55700K .......... .......... .......... .......... .......... 20% 11.5M 17s
55750K .......... .......... .......... .......... .......... 21% 43.9M 17s
55800K .......... .......... .......... .......... .......... 21% 11.9M 17s
55850K .......... .......... .......... .......... .......... 21% 10.6M 17s
55900K .......... .......... .......... .......... .......... 21% 11.9M 17s
55950K .......... .......... .......... .......... .......... 21% 11.1M 17s
56000K .......... .......... .......... .......... .......... 21% 12.7M 17s
56050K .......... .......... .......... .......... .......... 21% 122M 17s
56100K .......... .......... .......... .......... .......... 21% 14.1M 17s
56150K .......... .......... .......... .......... .......... 21% 9.56M 17s
56200K .......... .......... .......... .......... .......... 21% 28.2M 17s
56250K .......... .......... .......... .......... .......... 21% 15.8M 17s
56300K .......... .......... .......... .......... .......... 21% 13.1M 17s
56350K .......... .......... .......... .......... .......... 21% 11.4M 17s
56400K .......... .......... .......... .......... .......... 21% 31.1M 17s
56450K .......... .......... .......... .......... .......... 21% 11.1M 17s
56500K .......... .......... .......... .......... .......... 21% 16.9M 17s
56550K .......... .......... .......... .......... .......... 21% 12.6M 17s
56600K .......... .......... .......... .......... .......... 21% 20.7M 17s
56650K .......... .......... .......... .......... .......... 21% 6.65M 17s
56700K .......... .......... .......... .......... .......... 21% 59.2M 17s
56750K .......... .......... .......... .......... .......... 21% 44.4M 17s
56800K .......... .......... .......... .......... .......... 21% 13.1M 17s
56850K .......... .......... .......... .......... .......... 21% 12.0M 17s
56900K .......... .......... .......... .......... .......... 21% 9.48M 17s
56950K .......... .......... .......... .......... .......... 21% 8.31M 17s
57000K .......... .......... .......... .......... .......... 21% 30.6M 17s
57050K .......... .......... .......... .......... .......... 21% 11.7M 17s
57100K .......... .......... .......... .......... .......... 21% 9.07M 17s
57150K .......... .......... .......... .......... .......... 21% 12.0M 17s
57200K .......... .......... .......... .......... .......... 21% 10.3M 17s
57250K .......... .......... .......... .......... .......... 21% 13.3M 17s
57300K .......... .......... .......... .......... .......... 21% 10.4M 17s
57350K .......... .......... .......... .......... .......... 21% 12.4M 17s
57400K .......... .......... .......... .......... .......... 21% 18.9M 17s
57450K .......... .......... .......... .......... .......... 21% 8.80M 17s
57500K .......... .......... .......... .......... .......... 21% 21.7M 17s
57550K .......... .......... .......... .......... .......... 21% 13.2M 17s
57600K .......... .......... .......... .......... .......... 21% 11.7M 17s
57650K .......... .......... .......... .......... .......... 21% 12.9M 17s
57700K .......... .......... .......... .......... .......... 21% 8.80M 17s
57750K .......... .......... .......... .......... .......... 21% 24.0M 17s
57800K .......... .......... .......... .......... .......... 21% 11.9M 17s
57850K .......... .......... .......... .......... .......... 21% 11.7M 17s
57900K .......... .......... .......... .......... .......... 21% 16.7M 17s
57950K .......... .......... .......... .......... .......... 21% 16.2M 17s
58000K .......... .......... .......... .......... .......... 21% 11.9M 17s
58050K .......... .......... .......... .......... .......... 21% 12.2M 17s
58100K .......... .......... .......... .......... .......... 21% 12.5M 17s
58150K .......... .......... .......... .......... .......... 21% 28.9M 17s
58200K .......... .......... .......... .......... .......... 21% 17.6M 17s
58250K .......... .......... .......... .......... .......... 21% 11.2M 17s
58300K .......... .......... .......... .......... .......... 21% 15.0M 17s
58350K .......... .......... .......... .......... .......... 21% 16.9M 17s
58400K .......... .......... .......... .......... .......... 22% 24.7M 17s
58450K .......... .......... .......... .......... .......... 22% 11.7M 17s
58500K .......... .......... .......... .......... .......... 22% 12.2M 17s
58550K .......... .......... .......... .......... .......... 22% 36.0M 17s
58600K .......... .......... .......... .......... .......... 22% 17.1M 17s
58650K .......... .......... .......... .......... .......... 22% 11.1M 17s
58700K .......... .......... .......... .......... .......... 22% 11.5M 17s
58750K .......... .......... .......... .......... .......... 22% 33.1M 17s
58800K .......... .......... .......... .......... .......... 22% 16.0M 17s
58850K .......... .......... .......... .......... .......... 22% 12.0M 17s
58900K .......... .......... .......... .......... .......... 22% 10.8M 17s
58950K .......... .......... .......... .......... .......... 22% 76.3M 17s
59000K .......... .......... .......... .......... .......... 22% 11.7M 17s
59050K .......... .......... .......... .......... .......... 22% 13.6M 17s
59100K .......... .......... .......... .......... .......... 22% 12.8M 17s
59150K .......... .......... .......... .......... .......... 22% 11.2M 17s
59200K .......... .......... .......... .......... .......... 22% 15.4M 17s
59250K .......... .......... .......... .......... .......... 22% 15.3M 17s
59300K .......... .......... .......... .......... .......... 22% 13.1M 17s
59350K .......... .......... .......... .......... .......... 22% 9.93M 17s
59400K .......... .......... .......... .......... .......... 22% 12.6M 17s
59450K .......... .......... .......... .......... .......... 22% 11.2M 17s
59500K .......... .......... .......... .......... .......... 22% 25.7M 16s
59550K .......... .......... .......... .......... .......... 22% 10.8M 16s
59600K .......... .......... .......... .......... .......... 22% 13.5M 16s
59650K .......... .......... .......... .......... .......... 22% 12.4M 16s
59700K .......... .......... .......... .......... .......... 22% 11.0M 16s
59750K .......... .......... .......... .......... .......... 22% 10.1M 16s
59800K .......... .......... .......... .......... .......... 22% 12.1M 16s
59850K .......... .......... .......... .......... .......... 22% 12.0M 16s
59900K .......... .......... .......... .......... .......... 22% 16.6M 16s
59950K .......... .......... .......... .......... .......... 22% 12.9M 16s
60000K .......... .......... .......... .......... .......... 22% 23.4M 16s
60050K .......... .......... .......... .......... .......... 22% 14.9M 16s
60100K .......... .......... .......... .......... .......... 22% 11.9M 16s
60150K .......... .......... .......... .......... .......... 22% 14.7M 16s
60200K .......... .......... .......... .......... .......... 22% 16.2M 16s
60250K .......... .......... .......... .......... .......... 22% 19.7M 16s
60300K .......... .......... .......... .......... .......... 22% 12.2M 16s
60350K .......... .......... .......... .......... .......... 22% 13.5M 16s
60400K .......... .......... .......... .......... .......... 22% 12.6M 16s
60450K .......... .......... .......... .......... .......... 22% 14.5M 16s
60500K .......... .......... .......... .......... .......... 22% 21.1M 16s
60550K .......... .......... .......... .......... .......... 22% 12.9M 16s
60600K .......... .......... .......... .......... .......... 22% 13.1M 16s
60650K .......... .......... .......... .......... .......... 22% 12.7M 16s
60700K .......... .......... .......... .......... .......... 22% 24.0M 16s
60750K .......... .......... .......... .......... .......... 22% 13.7M 16s
60800K .......... .......... .......... .......... .......... 22% 12.8M 16s
60850K .......... .......... .......... .......... .......... 22% 62.2M 16s
60900K .......... .......... .......... .......... .......... 22% 12.2M 16s
60950K .......... .......... .......... .......... .......... 22% 12.0M 16s
61000K .......... .......... .......... .......... .......... 22% 15.2M 16s
61050K .......... .......... .......... .......... .......... 23% 58.6M 16s
61100K .......... .......... .......... .......... .......... 23% 11.5M 16s
61150K .......... .......... .......... .......... .......... 23% 13.8M 16s
61200K .......... .......... .......... .......... .......... 23% 16.5M 16s
61250K .......... .......... .......... .......... .......... 23% 20.3M 16s
61300K .......... .......... .......... .......... .......... 23% 13.2M 16s
61350K .......... .......... .......... .......... .......... 23% 16.3M 16s
61400K .......... .......... .......... .......... .......... 23% 13.0M 16s
61450K .......... .......... .......... .......... .......... 23% 23.5M 16s
61500K .......... .......... .......... .......... .......... 23% 12.6M 16s
61550K .......... .......... .......... .......... .......... 23% 15.3M 16s
61600K .......... .......... .......... .......... .......... 23% 12.6M 16s
61650K .......... .......... .......... .......... .......... 23% 21.2M 16s
61700K .......... .......... .......... .......... .......... 23% 10.5M 16s
61750K .......... .......... .......... .......... .......... 23% 17.0M 16s
61800K .......... .......... .......... .......... .......... 23% 41.4M 16s
61850K .......... .......... .......... .......... .......... 23% 13.5M 16s
61900K .......... .......... .......... .......... .......... 23% 14.6M 16s
61950K .......... .......... .......... .......... .......... 23% 16.6M 16s
62000K .......... .......... .......... .......... .......... 23% 20.4M 16s
62050K .......... .......... .......... .......... .......... 23% 19.2M 16s
62100K .......... .......... .......... .......... .......... 23% 12.9M 16s
62150K .......... .......... .......... .......... .......... 23% 40.4M 16s
62200K .......... .......... .......... .......... .......... 23% 14.7M 16s
62250K .......... .......... .......... .......... .......... 23% 12.1M 16s
62300K .......... .......... .......... .......... .......... 23% 46.2M 16s
62350K .......... .......... .......... .......... .......... 23% 13.7M 16s
62400K .......... .......... .......... .......... .......... 23% 6.54M 16s
62450K .......... .......... .......... .......... .......... 23% 186M 16s
62500K .......... .......... .......... .......... .......... 23% 17.6M 16s
62550K .......... .......... .......... .......... .......... 23% 13.2M 16s
62600K .......... .......... .......... .......... .......... 23% 57.8M 16s
62650K .......... .......... .......... .......... .......... 23% 13.7M 16s
62700K .......... .......... .......... .......... .......... 23% 12.3M 16s
62750K .......... .......... .......... .......... .......... 23% 12.0M 16s
62800K .......... .......... .......... .......... .......... 23% 7.11M 16s
62850K .......... .......... .......... .......... .......... 23% 9.05M 16s
62900K .......... .......... .......... .......... .......... 23% 12.8M 16s
62950K .......... .......... .......... .......... .......... 23% 10.8M 16s
63000K .......... .......... .......... .......... .......... 23% 11.4M 16s
63050K .......... .......... .......... .......... .......... 23% 11.1M 16s
63100K .......... .......... .......... .......... .......... 23% 7.38M 16s
63150K .......... .......... .......... .......... .......... 23% 10.5M 16s
63200K .......... .......... .......... .......... .......... 23% 10.5M 16s
63250K .......... .......... .......... .......... .......... 23% 10.1M 16s
63300K .......... .......... .......... .......... .......... 23% 11.0M 16s
63350K .......... .......... .......... .......... .......... 23% 10.9M 16s
63400K .......... .......... .......... .......... .......... 23% 13.9M 16s
63450K .......... .......... .......... .......... .......... 23% 10.5M 16s
63500K .......... .......... .......... .......... .......... 23% 11.4M 16s
63550K .......... .......... .......... .......... .......... 23% 10.4M 16s
63600K .......... .......... .......... .......... .......... 23% 11.5M 16s
63650K .......... .......... .......... .......... .......... 23% 12.3M 16s
63700K .......... .......... .......... .......... .......... 24% 10.7M 16s
63750K .......... .......... .......... .......... .......... 24% 15.0M 16s
63800K .......... .......... .......... .......... .......... 24% 9.92M 16s
63850K .......... .......... .......... .......... .......... 24% 13.2M 16s
63900K .......... .......... .......... .......... .......... 24% 21.2M 16s
63950K .......... .......... .......... .......... .......... 24% 10.2M 16s
64000K .......... .......... .......... .......... .......... 24% 10.4M 16s
64050K .......... .......... .......... .......... .......... 24% 16.7M 16s
64100K .......... .......... .......... .......... .......... 24% 9.58M 16s
64150K .......... .......... .......... .......... .......... 24% 18.9M 16s
64200K .......... .......... .......... .......... .......... 24% 9.47M 16s
64250K .......... .......... .......... .......... .......... 24% 11.3M 16s
64300K .......... .......... .......... .......... .......... 24% 12.5M 16s
64350K .......... .......... .......... .......... .......... 24% 13.0M 16s
64400K .......... .......... .......... .......... .......... 24% 5.23M 16s
64450K .......... .......... .......... .......... .......... 24% 78.0M 16s
64500K .......... .......... .......... .......... .......... 24% 22.4M 16s
64550K .......... .......... .......... .......... .......... 24% 9.50M 16s
64600K .......... .......... .......... .......... .......... 24% 9.17M 16s
64650K .......... .......... .......... .......... .......... 24% 10.4M 16s
64700K .......... .......... .......... .......... .......... 24% 11.0M 16s
64750K .......... .......... .......... .......... .......... 24% 9.99M 16s
64800K .......... .......... .......... .......... .......... 24% 14.3M 16s
64850K .......... .......... .......... .......... .......... 24% 9.01M 16s
64900K .......... .......... .......... .......... .......... 24% 13.5M 16s
64950K .......... .......... .......... .......... .......... 24% 8.52M 16s
65000K .......... .......... .......... .......... .......... 24% 11.6M 16s
65050K .......... .......... .......... .......... .......... 24% 11.2M 16s
65100K .......... .......... .......... .......... .......... 24% 7.85M 16s
65150K .......... .......... .......... .......... .......... 24% 13.0M 16s
65200K .......... .......... .......... .......... .......... 24% 13.7M 16s
65250K .......... .......... .......... .......... .......... 24% 7.97M 16s
65300K .......... .......... .......... .......... .......... 24% 10.7M 16s
65350K .......... .......... .......... .......... .......... 24% 11.4M 16s
65400K .......... .......... .......... .......... .......... 24% 13.9M 16s
65450K .......... .......... .......... .......... .......... 24% 11.7M 16s
65500K .......... .......... .......... .......... .......... 24% 13.2M 16s
65550K .......... .......... .......... .......... .......... 24% 13.5M 16s
65600K .......... .......... .......... .......... .......... 24% 5.09M 16s
65650K .......... .......... .......... .......... .......... 24% 77.3M 16s
65700K .......... .......... .......... .......... .......... 24% 8.46M 16s
65750K .......... .......... .......... .......... .......... 24% 9.53M 16s
65800K .......... .......... .......... .......... .......... 24% 9.01M 16s
65850K .......... .......... .......... .......... .......... 24% 8.35M 16s
65900K .......... .......... .......... .......... .......... 24% 7.39M 16s
65950K .......... .......... .......... .......... .......... 24% 10.2M 16s
66000K .......... .......... .......... .......... .......... 24% 7.70M 16s
66050K .......... .......... .......... .......... .......... 24% 6.64M 16s
66100K .......... .......... .......... .......... .......... 24% 9.09M 16s
66150K .......... .......... .......... .......... .......... 24% 11.0M 16s
66200K .......... .......... .......... .......... .......... 24% 5.71M 16s
66250K .......... .......... .......... .......... .......... 24% 10.1M 16s
66300K .......... .......... .......... .......... .......... 24% 9.23M 16s
66350K .......... .......... .......... .......... .......... 25% 11.1M 16s
66400K .......... .......... .......... .......... .......... 25% 9.26M 16s
66450K .......... .......... .......... .......... .......... 25% 12.3M 16s
66500K .......... .......... .......... .......... .......... 25% 15.0M 16s
66550K .......... .......... .......... .......... .......... 25% 11.9M 16s
66600K .......... .......... .......... .......... .......... 25% 11.6M 16s
66650K .......... .......... .......... .......... .......... 25% 11.4M 16s
66700K .......... .......... .......... .......... .......... 25% 11.9M 16s
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66800K .......... .......... .......... .......... .......... 25% 12.9M 16s
66850K .......... .......... .......... .......... .......... 25% 12.0M 16s
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67000K .......... .......... .......... .......... .......... 25% 12.2M 16s
67050K .......... .......... .......... .......... .......... 25% 12.0M 16s
67100K .......... .......... .......... .......... .......... 25% 8.81M 16s
67150K .......... .......... .......... .......... .......... 25% 15.0M 16s
67200K .......... .......... .......... .......... .......... 25% 4.66M 16s
67250K .......... .......... .......... .......... .......... 25% 197M 16s
67300K .......... .......... .......... .......... .......... 25% 46.7M 16s
67350K .......... .......... .......... .......... .......... 25% 8.23M 16s
67400K .......... .......... .......... .......... .......... 25% 12.6M 16s
67450K .......... .......... .......... .......... .......... 25% 7.43M 16s
67500K .......... .......... .......... .......... .......... 25% 10.4M 16s
67550K .......... .......... .......... .......... .......... 25% 16.3M 16s
67600K .......... .......... .......... .......... .......... 25% 10.3M 16s
67650K .......... .......... .......... .......... .......... 25% 7.87M 16s
67700K .......... .......... .......... .......... .......... 25% 13.1M 16s
67750K .......... .......... .......... .......... .......... 25% 10.8M 16s
67800K .......... .......... .......... .......... .......... 25% 15.8M 16s
67850K .......... .......... .......... .......... .......... 25% 15.1M 16s
67900K .......... .......... .......... .......... .......... 25% 13.3M 16s
67950K .......... .......... .......... .......... .......... 25% 17.9M 16s
68000K .......... .......... .......... .......... .......... 25% 11.3M 16s
68050K .......... .......... .......... .......... .......... 25% 21.6M 16s
68100K .......... .......... .......... .......... .......... 25% 12.2M 16s
68150K .......... .......... .......... .......... .......... 25% 15.8M 16s
68200K .......... .......... .......... .......... .......... 25% 8.44M 16s
68250K .......... .......... .......... .......... .......... 25% 24.5M 16s
68300K .......... .......... .......... .......... .......... 25% 9.30M 16s
68350K .......... .......... .......... .......... .......... 25% 14.8M 16s
68400K .......... .......... .......... .......... .......... 25% 17.4M 16s
68450K .......... .......... .......... .......... .......... 25% 9.16M 16s
68500K .......... .......... .......... .......... .......... 25% 12.6M 16s
68550K .......... .......... .......... .......... .......... 25% 12.2M 16s
68600K .......... .......... .......... .......... .......... 25% 15.9M 16s
68650K .......... .......... .......... .......... .......... 25% 9.57M 16s
68700K .......... .......... .......... .......... .......... 25% 8.70M 16s
68750K .......... .......... .......... .......... .......... 25% 18.8M 16s
68800K .......... .......... .......... .......... .......... 25% 14.4M 16s
68850K .......... .......... .......... .......... .......... 25% 9.33M 16s
68900K .......... .......... .......... .......... .......... 25% 8.29M 16s
68950K .......... .......... .......... .......... .......... 25% 16.6M 16s
69000K .......... .......... .......... .......... .......... 26% 7.07M 16s
69050K .......... .......... .......... .......... .......... 26% 18.2M 16s
69100K .......... .......... .......... .......... .......... 26% 9.77M 16s
69150K .......... .......... .......... .......... .......... 26% 8.33M 16s
69200K .......... .......... .......... .......... .......... 26% 16.4M 16s
69250K .......... .......... .......... .......... .......... 26% 8.10M 16s
69300K .......... .......... .......... .......... .......... 26% 8.26M 16s
69350K .......... .......... .......... .......... .......... 26% 7.00M 16s
69400K .......... .......... .......... .......... .......... 26% 8.55M 16s
69450K .......... .......... .......... .......... .......... 26% 8.75M 16s
69500K .......... .......... .......... .......... .......... 26% 8.41M 16s
69550K .......... .......... .......... .......... .......... 26% 8.73M 16s
69600K .......... .......... .......... .......... .......... 26% 12.7M 16s
69650K .......... .......... .......... .......... .......... 26% 15.5M 16s
69700K .......... .......... .......... .......... .......... 26% 9.34M 16s
69750K .......... .......... .......... .......... .......... 26% 15.6M 16s
69800K .......... .......... .......... .......... .......... 26% 14.9M 16s
69850K .......... .......... .......... .......... .......... 26% 15.9M 16s
69900K .......... .......... .......... .......... .......... 26% 17.3M 16s
69950K .......... .......... .......... .......... .......... 26% 16.2M 16s
70000K .......... .......... .......... .......... .......... 26% 8.61M 16s
70050K .......... .......... .......... .......... .......... 26% 16.7M 16s
70100K .......... .......... .......... .......... .......... 26% 11.0M 16s
70150K .......... .......... .......... .......... .......... 26% 39.1M 16s
70200K .......... .......... .......... .......... .......... 26% 9.12M 16s
70250K .......... .......... .......... .......... .......... 26% 13.1M 16s
70300K .......... .......... .......... .......... .......... 26% 9.48M 16s
70350K .......... .......... .......... .......... .......... 26% 14.0M 16s
70400K .......... .......... .......... .......... .......... 26% 9.35M 16s
70450K .......... .......... .......... .......... .......... 26% 9.76M 16s
70500K .......... .......... .......... .......... .......... 26% 11.7M 16s
70550K .......... .......... .......... .......... .......... 26% 12.9M 16s
70600K .......... .......... .......... .......... .......... 26% 10.9M 16s
70650K .......... .......... .......... .......... .......... 26% 18.2M 16s
70700K .......... .......... .......... .......... .......... 26% 6.04M 16s
70750K .......... .......... .......... .......... .......... 26% 61.8M 16s
70800K .......... .......... .......... .......... .......... 26% 18.8M 16s
70850K .......... .......... .......... .......... .......... 26% 12.9M 16s
70900K .......... .......... .......... .......... .......... 26% 9.69M 16s
70950K .......... .......... .......... .......... .......... 26% 21.1M 16s
71000K .......... .......... .......... .......... .......... 26% 15.9M 16s
71050K .......... .......... .......... .......... .......... 26% 17.8M 16s
71100K .......... .......... .......... .......... .......... 26% 11.2M 16s
71150K .......... .......... .......... .......... .......... 26% 15.9M 16s
71200K .......... .......... .......... .......... .......... 26% 10.9M 16s
71250K .......... .......... .......... .......... .......... 26% 14.7M 16s
71300K .......... .......... .......... .......... .......... 26% 17.8M 16s
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71400K .......... .......... .......... .......... .......... 26% 15.6M 16s
71450K .......... .......... .......... .......... .......... 26% 13.4M 16s
71500K .......... .......... .......... .......... .......... 26% 13.3M 16s
71550K .......... .......... .......... .......... .......... 26% 13.1M 16s
71600K .......... .......... .......... .......... .......... 26% 15.3M 16s
71650K .......... .......... .......... .......... .......... 27% 16.0M 16s
71700K .......... .......... .......... .......... .......... 27% 10.8M 16s
71750K .......... .......... .......... .......... .......... 27% 14.7M 16s
71800K .......... .......... .......... .......... .......... 27% 13.3M 16s
71850K .......... .......... .......... .......... .......... 27% 12.9M 16s
71900K .......... .......... .......... .......... .......... 27% 13.2M 16s
71950K .......... .......... .......... .......... .......... 27% 10.4M 16s
72000K .......... .......... .......... .......... .......... 27% 13.1M 16s
72050K .......... .......... .......... .......... .......... 27% 9.57M 16s
72100K .......... .......... .......... .......... .......... 27% 26.0M 16s
72150K .......... .......... .......... .......... .......... 27% 18.1M 15s
72200K .......... .......... .......... .......... .......... 27% 8.04M 16s
72250K .......... .......... .......... .......... .......... 27% 29.0M 15s
72300K .......... .......... .......... .......... .......... 27% 16.7M 15s
72350K .......... .......... .......... .......... .......... 27% 6.28M 15s
72400K .......... .......... .......... .......... .......... 27% 39.9M 15s
72450K .......... .......... .......... .......... .......... 27% 11.4M 15s
72500K .......... .......... .......... .......... .......... 27% 12.0M 15s
72550K .......... .......... .......... .......... .......... 27% 15.3M 15s
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72700K .......... .......... .......... .......... .......... 27% 11.0M 15s
72750K .......... .......... .......... .......... .......... 27% 17.5M 15s
72800K .......... .......... .......... .......... .......... 27% 14.8M 15s
72850K .......... .......... .......... .......... .......... 27% 13.8M 15s
72900K .......... .......... .......... .......... .......... 27% 14.8M 15s
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73000K .......... .......... .......... .......... .......... 27% 13.5M 15s
73050K .......... .......... .......... .......... .......... 27% 13.8M 15s
73100K .......... .......... .......... .......... .......... 27% 13.1M 15s
73150K .......... .......... .......... .......... .......... 27% 13.1M 15s
73200K .......... .......... .......... .......... .......... 27% 12.0M 15s
73250K .......... .......... .......... .......... .......... 27% 12.9M 15s
73300K .......... .......... .......... .......... .......... 27% 12.3M 15s
73350K .......... .......... .......... .......... .......... 27% 10.8M 15s
73400K .......... .......... .......... .......... .......... 27% 16.1M 15s
73450K .......... .......... .......... .......... .......... 27% 12.7M 15s
73500K .......... .......... .......... .......... .......... 27% 12.0M 15s
73550K .......... .......... .......... .......... .......... 27% 12.1M 15s
73600K .......... .......... .......... .......... .......... 27% 12.4M 15s
73650K .......... .......... .......... .......... .......... 27% 23.0M 15s
73700K .......... .......... .......... .......... .......... 27% 8.34M 15s
73750K .......... .......... .......... .......... .......... 27% 11.6M 15s
73800K .......... .......... .......... .......... .......... 27% 12.8M 15s
73850K .......... .......... .......... .......... .......... 27% 25.5M 15s
73900K .......... .......... .......... .......... .......... 27% 11.0M 15s
73950K .......... .......... .......... .......... .......... 27% 10.9M 15s
74000K .......... .......... .......... .......... .......... 27% 19.3M 15s
74050K .......... .......... .......... .......... .......... 27% 16.0M 15s
74100K .......... .......... .......... .......... .......... 27% 11.3M 15s
74150K .......... .......... .......... .......... .......... 27% 25.8M 15s
74200K .......... .......... .......... .......... .......... 27% 15.6M 15s
74250K .......... .......... .......... .......... .......... 27% 11.7M 15s
74300K .......... .......... .......... .......... .......... 28% 13.7M 15s
74350K .......... .......... .......... .......... .......... 28% 13.5M 15s
74400K .......... .......... .......... .......... .......... 28% 26.2M 15s
74450K .......... .......... .......... .......... .......... 28% 9.28M 15s
74500K .......... .......... .......... .......... .......... 28% 6.70M 15s
74550K .......... .......... .......... .......... .......... 28% 20.6M 15s
74600K .......... .......... .......... .......... .......... 28% 22.5M 15s
74650K .......... .......... .......... .......... .......... 28% 27.1M 15s
74700K .......... .......... .......... .......... .......... 28% 11.4M 15s
74750K .......... .......... .......... .......... .......... 28% 17.0M 15s
74800K .......... .......... .......... .......... .......... 28% 11.9M 15s
74850K .......... .......... .......... .......... .......... 28% 10.1M 15s
74900K .......... .......... .......... .......... .......... 28% 12.2M 15s
74950K .......... .......... .......... .......... .......... 28% 11.9M 15s
75000K .......... .......... .......... .......... .......... 28% 10.2M 15s
75050K .......... .......... .......... .......... .......... 28% 14.9M 15s
75100K .......... .......... .......... .......... .......... 28% 4.60M 15s
75150K .......... .......... .......... .......... .......... 28% 53.2M 15s
75200K .......... .......... .......... .......... .......... 28% 9.46M 15s
75250K .......... .......... .......... .......... .......... 28% 6.78M 15s
75300K .......... .......... .......... .......... .......... 28% 15.9M 15s
75350K .......... .......... .......... .......... .......... 28% 5.34M 15s
75400K .......... .......... .......... .......... .......... 28% 6.34M 15s
75450K .......... .......... .......... .......... .......... 28% 6.14M 15s
75500K .......... .......... .......... .......... .......... 28% 6.26M 15s
75550K .......... .......... .......... .......... .......... 28% 11.1M 15s
75600K .......... .......... .......... .......... .......... 28% 7.20M 15s
75650K .......... .......... .......... .......... .......... 28% 9.26M 15s
75700K .......... .......... .......... .......... .......... 28% 4.42M 15s
75750K .......... .......... .......... .......... .......... 28% 14.0M 15s
75800K .......... .......... .......... .......... .......... 28% 7.77M 15s
75850K .......... .......... .......... .......... .......... 28% 6.78M 15s
75900K .......... .......... .......... .......... .......... 28% 6.05M 15s
75950K .......... .......... .......... .......... .......... 28% 6.22M 15s
76000K .......... .......... .......... .......... .......... 28% 5.82M 15s
76050K .......... .......... .......... .......... .......... 28% 8.32M 15s
76100K .......... .......... .......... .......... .......... 28% 6.03M 15s
76150K .......... .......... .......... .......... .......... 28% 7.74M 15s
76200K .......... .......... .......... .......... .......... 28% 5.98M 15s
76250K .......... .......... .......... .......... .......... 28% 11.4M 15s
76300K .......... .......... .......... .......... .......... 28% 5.73M 15s
76350K .......... .......... .......... .......... .......... 28% 11.9M 15s
76400K .......... .......... .......... .......... .......... 28% 7.94M 15s
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76500K .......... .......... .......... .......... .......... 28% 13.4M 15s
76550K .......... .......... .......... .......... .......... 28% 6.47M 15s
76600K .......... .......... .......... .......... .......... 28% 12.1M 15s
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76700K .......... .......... .......... .......... .......... 28% 10.7M 15s
76750K .......... .......... .......... .......... .......... 28% 17.4M 15s
76800K .......... .......... .......... .......... .......... 28% 7.26M 15s
76850K .......... .......... .......... .......... .......... 28% 10.1M 15s
76900K .......... .......... .......... .......... .......... 28% 14.2M 15s
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77000K .......... .......... .......... .......... .......... 29% 12.6M 15s
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77100K .......... .......... .......... .......... .......... 29% 13.3M 15s
77150K .......... .......... .......... .......... .......... 29% 7.72M 15s
77200K .......... .......... .......... .......... .......... 29% 12.8M 15s
77250K .......... .......... .......... .......... .......... 29% 12.2M 15s
77300K .......... .......... .......... .......... .......... 29% 11.7M 15s
77350K .......... .......... .......... .......... .......... 29% 12.8M 15s
77400K .......... .......... .......... .......... .......... 29% 12.7M 15s
77450K .......... .......... .......... .......... .......... 29% 8.78M 15s
77500K .......... .......... .......... .......... .......... 29% 12.7M 15s
77550K .......... .......... .......... .......... .......... 29% 17.0M 15s
77600K .......... .......... .......... .......... .......... 29% 8.83M 15s
77650K .......... .......... .......... .......... .......... 29% 4.92M 15s
77700K .......... .......... .......... .......... .......... 29% 52.6M 15s
77750K .......... .......... .......... .......... .......... 29% 12.2M 15s
77800K .......... .......... .......... .......... .......... 29% 10.1M 15s
77850K .......... .......... .......... .......... .......... 29% 6.67M 15s
77900K .......... .......... .......... .......... .......... 29% 11.1M 15s
77950K .......... .......... .......... .......... .......... 29% 7.94M 15s
78000K .......... .......... .......... .......... .......... 29% 8.91M 15s
78050K .......... .......... .......... .......... .......... 29% 10.4M 15s
78100K .......... .......... .......... .......... .......... 29% 7.93M 15s
78150K .......... .......... .......... .......... .......... 29% 11.4M 15s
78200K .......... .......... .......... .......... .......... 29% 8.73M 15s
78250K .......... .......... .......... .......... .......... 29% 12.8M 15s
78300K .......... .......... .......... .......... .......... 29% 12.7M 15s
78350K .......... .......... .......... .......... .......... 29% 12.2M 15s
78400K .......... .......... .......... .......... .......... 29% 14.3M 15s
78450K .......... .......... .......... .......... .......... 29% 9.09M 15s
78500K .......... .......... .......... .......... .......... 29% 12.6M 15s
78550K .......... .......... .......... .......... .......... 29% 24.1M 15s
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78700K .......... .......... .......... .......... .......... 29% 11.1M 15s
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78900K .......... .......... .......... .......... .......... 29% 12.6M 15s
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79000K .......... .......... .......... .......... .......... 29% 24.3M 15s
79050K .......... .......... .......... .......... .......... 29% 11.1M 15s
79100K .......... .......... .......... .......... .......... 29% 12.0M 15s
79150K .......... .......... .......... .......... .......... 29% 10.5M 15s
79200K .......... .......... .......... .......... .......... 29% 11.8M 15s
79250K .......... .......... .......... .......... .......... 29% 13.4M 15s
79300K .......... .......... .......... .......... .......... 29% 13.9M 15s
79350K .......... .......... .......... .......... .......... 29% 10.6M 15s
79400K .......... .......... .......... .......... .......... 29% 27.3M 15s
79450K .......... .......... .......... .......... .......... 29% 8.50M 15s
79500K .......... .......... .......... .......... .......... 29% 48.8M 15s
79550K .......... .......... .......... .......... .......... 29% 13.5M 15s
79600K .......... .......... .......... .......... .......... 29% 11.7M 15s
79650K .......... .......... .......... .......... .......... 30% 12.4M 15s
79700K .......... .......... .......... .......... .......... 30% 11.9M 15s
79750K .......... .......... .......... .......... .......... 30% 12.9M 15s
79800K .......... .......... .......... .......... .......... 30% 71.8M 15s
79850K .......... .......... .......... .......... .......... 30% 9.12M 15s
79900K .......... .......... .......... .......... .......... 30% 19.1M 15s
79950K .......... .......... .......... .......... .......... 30% 11.6M 15s
80000K .......... .......... .......... .......... .......... 30% 14.4M 15s
80050K .......... .......... .......... .......... .......... 30% 12.5M 15s
80100K .......... .......... .......... .......... .......... 30% 43.6M 15s
80150K .......... .......... .......... .......... .......... 30% 12.5M 15s
80200K .......... .......... .......... .......... .......... 30% 14.5M 15s
80250K .......... .......... .......... .......... .......... 30% 12.8M 15s
80300K .......... .......... .......... .......... .......... 30% 29.5M 15s
80350K .......... .......... .......... .......... .......... 30% 16.2M 15s
80400K .......... .......... .......... .......... .......... 30% 14.8M 15s
80450K .......... .......... .......... .......... .......... 30% 11.5M 15s
80500K .......... .......... .......... .......... .......... 30% 22.2M 15s
80550K .......... .......... .......... .......... .......... 30% 19.2M 15s
80600K .......... .......... .......... .......... .......... 30% 15.7M 15s
80650K .......... .......... .......... .......... .......... 30% 25.1M 15s
80700K .......... .......... .......... .......... .......... 30% 13.0M 15s
80750K .......... .......... .......... .......... .......... 30% 6.65M 15s
80800K .......... .......... .......... .......... .......... 30% 51.7M 15s
80850K .......... .......... .......... .......... .......... 30% 15.9M 15s
80900K .......... .......... .......... .......... .......... 30% 13.8M 15s
80950K .......... .......... .......... .......... .......... 30% 10.9M 15s
81000K .......... .......... .......... .......... .......... 30% 12.9M 15s
81050K .......... .......... .......... .......... .......... 30% 16.2M 15s
81100K .......... .......... .......... .......... .......... 30% 10.8M 15s
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81250K .......... .......... .......... .......... .......... 30% 13.5M 15s
81300K .......... .......... .......... .......... .......... 30% 11.0M 15s
81350K .......... .......... .......... .......... .......... 30% 9.00M 15s
81400K .......... .......... .......... .......... .......... 30% 12.9M 15s
81450K .......... .......... .......... .......... .......... 30% 13.7M 15s
81500K .......... .......... .......... .......... .......... 30% 13.3M 15s
81550K .......... .......... .......... .......... .......... 30% 14.3M 15s
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81650K .......... .......... .......... .......... .......... 30% 14.4M 15s
81700K .......... .......... .......... .......... .......... 30% 12.7M 15s
81750K .......... .......... .......... .......... .......... 30% 21.0M 15s
81800K .......... .......... .......... .......... .......... 30% 13.5M 15s
81850K .......... .......... .......... .......... .......... 30% 17.0M 15s
81900K .......... .......... .......... .......... .......... 30% 15.3M 15s
81950K .......... .......... .......... .......... .......... 30% 12.8M 15s
82000K .......... .......... .......... .......... .......... 30% 19.8M 15s
82050K .......... .......... .......... .......... .......... 30% 30.2M 15s
82100K .......... .......... .......... .......... .......... 30% 12.3M 15s
82150K .......... .......... .......... .......... .......... 30% 11.9M 15s
82200K .......... .......... .......... .......... .......... 30% 14.4M 15s
82250K .......... .......... .......... .......... .......... 30% 15.1M 15s
82300K .......... .......... .......... .......... .......... 31% 32.2M 15s
82350K .......... .......... .......... .......... .......... 31% 11.9M 15s
82400K .......... .......... .......... .......... .......... 31% 12.2M 15s
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82500K .......... .......... .......... .......... .......... 31% 27.4M 15s
82550K .......... .......... .......... .......... .......... 31% 17.2M 15s
82600K .......... .......... .......... .......... .......... 31% 11.9M 15s
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82700K .......... .......... .......... .......... .......... 31% 11.7M 15s
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82800K .......... .......... .......... .......... .......... 31% 18.9M 15s
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82900K .......... .......... .......... .......... .......... 31% 7.77M 15s
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83000K .......... .......... .......... .......... .......... 31% 12.5M 15s
83050K .......... .......... .......... .......... .......... 31% 6.63M 15s
83100K .......... .......... .......... .......... .......... 31% 51.5M 15s
83150K .......... .......... .......... .......... .......... 31% 8.96M 15s
83200K .......... .......... .......... .......... .......... 31% 10.2M 15s
83250K .......... .......... .......... .......... .......... 31% 9.72M 15s
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83350K .......... .......... .......... .......... .......... 31% 14.3M 15s
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83450K .......... .......... .......... .......... .......... 31% 12.3M 15s
83500K .......... .......... .......... .......... .......... 31% 8.77M 15s
83550K .......... .......... .......... .......... .......... 31% 12.6M 15s
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83650K .......... .......... .......... .......... .......... 31% 11.8M 15s
83700K .......... .......... .......... .......... .......... 31% 10.9M 15s
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83800K .......... .......... .......... .......... .......... 31% 12.8M 15s
83850K .......... .......... .......... .......... .......... 31% 6.78M 15s
83900K .......... .......... .......... .......... .......... 31% 11.1M 15s
83950K .......... .......... .......... .......... .......... 31% 7.76M 15s
84000K .......... .......... .......... .......... .......... 31% 12.0M 15s
84050K .......... .......... .......... .......... .......... 31% 16.9M 15s
84100K .......... .......... .......... .......... .......... 31% 5.85M 15s
84150K .......... .......... .......... .......... .......... 31% 23.6M 15s
84200K .......... .......... .......... .......... .......... 31% 5.86M 15s
84250K .......... .......... .......... .......... .......... 31% 8.35M 15s
84300K .......... .......... .......... .......... .......... 31% 7.98M 15s
84350K .......... .......... .......... .......... .......... 31% 7.96M 15s
84400K .......... .......... .......... .......... .......... 31% 7.86M 15s
84450K .......... .......... .......... .......... .......... 31% 9.70M 15s
84500K .......... .......... .......... .......... .......... 31% 8.18M 15s
84550K .......... .......... .......... .......... .......... 31% 11.2M 15s
84600K .......... .......... .......... .......... .......... 31% 7.07M 15s
84650K .......... .......... .......... .......... .......... 31% 9.02M 15s
84700K .......... .......... .......... .......... .......... 31% 10.6M 15s
84750K .......... .......... .......... .......... .......... 31% 12.1M 15s
84800K .......... .......... .......... .......... .......... 31% 10.6M 15s
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84900K .......... .......... .......... .......... .......... 31% 10.5M 15s
84950K .......... .......... .......... .......... .......... 32% 6.17M 15s
85000K .......... .......... .......... .......... .......... 32% 22.1M 15s
85050K .......... .......... .......... .......... .......... 32% 9.34M 15s
85100K .......... .......... .......... .......... .......... 32% 10.1M 15s
85150K .......... .......... .......... .......... .......... 32% 13.6M 15s
85200K .......... .......... .......... .......... .......... 32% 13.1M 15s
85250K .......... .......... .......... .......... .......... 32% 12.6M 15s
85300K .......... .......... .......... .......... .......... 32% 9.68M 15s
85350K .......... .......... .......... .......... .......... 32% 12.5M 15s
85400K .......... .......... .......... .......... .......... 32% 13.2M 15s
85450K .......... .......... .......... .......... .......... 32% 10.0M 15s
85500K .......... .......... .......... .......... .......... 32% 14.5M 15s
85550K .......... .......... .......... .......... .......... 32% 11.4M 15s
85600K .......... .......... .......... .......... .......... 32% 9.64M 15s
85650K .......... .......... .......... .......... .......... 32% 11.2M 15s
85700K .......... .......... .......... .......... .......... 32% 11.2M 15s
85750K .......... .......... .......... .......... .......... 32% 10.9M 15s
85800K .......... .......... .......... .......... .......... 32% 10.3M 15s
85850K .......... .......... .......... .......... .......... 32% 11.3M 15s
85900K .......... .......... .......... .......... .......... 32% 11.8M 15s
85950K .......... .......... .......... .......... .......... 32% 5.64M 15s
86000K .......... .......... .......... .......... .......... 32% 192M 15s
86050K .......... .......... .......... .......... .......... 32% 8.68M 15s
86100K .......... .......... .......... .......... .......... 32% 8.91M 15s
86150K .......... .......... .......... .......... .......... 32% 11.5M 15s
86200K .......... .......... .......... .......... .......... 32% 6.56M 15s
86250K .......... .......... .......... .......... .......... 32% 9.80M 15s
86300K .......... .......... .......... .......... .......... 32% 8.48M 15s
86350K .......... .......... .......... .......... .......... 32% 8.10M 15s
86400K .......... .......... .......... .......... .......... 32% 8.80M 15s
86450K .......... .......... .......... .......... .......... 32% 6.01M 15s
86500K .......... .......... .......... .......... .......... 32% 8.88M 15s
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86600K .......... .......... .......... .......... .......... 32% 8.04M 15s
86650K .......... .......... .......... .......... .......... 32% 7.75M 15s
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86750K .......... .......... .......... .......... .......... 32% 7.50M 15s
86800K .......... .......... .......... .......... .......... 32% 10.1M 15s
86850K .......... .......... .......... .......... .......... 32% 5.56M 15s
86900K .......... .......... .......... .......... .......... 32% 7.34M 15s
86950K .......... .......... .......... .......... .......... 32% 6.96M 15s
87000K .......... .......... .......... .......... .......... 32% 8.73M 15s
87050K .......... .......... .......... .......... .......... 32% 8.12M 15s
87100K .......... .......... .......... .......... .......... 32% 7.29M 15s
87150K .......... .......... .......... .......... .......... 32% 11.1M 15s
87200K .......... .......... .......... .......... .......... 32% 7.72M 15s
87250K .......... .......... .......... .......... .......... 32% 8.18M 15s
87300K .......... .......... .......... .......... .......... 32% 11.7M 15s
87350K .......... .......... .......... .......... .......... 32% 7.52M 15s
87400K .......... .......... .......... .......... .......... 32% 11.3M 15s
87450K .......... .......... .......... .......... .......... 32% 10.4M 15s
87500K .......... .......... .......... .......... .......... 32% 11.2M 15s
87550K .......... .......... .......... .......... .......... 32% 7.68M 15s
87600K .......... .......... .......... .......... .......... 33% 8.41M 15s
87650K .......... .......... .......... .......... .......... 33% 12.8M 15s
87700K .......... .......... .......... .......... .......... 33% 10.1M 15s
87750K .......... .......... .......... .......... .......... 33% 12.7M 15s
87800K .......... .......... .......... .......... .......... 33% 11.0M 15s
87850K .......... .......... .......... .......... .......... 33% 12.8M 15s
87900K .......... .......... .......... .......... .......... 33% 10.7M 15s
87950K .......... .......... .......... .......... .......... 33% 10.1M 15s
88000K .......... .......... .......... .......... .......... 33% 11.2M 15s
88050K .......... .......... .......... .......... .......... 33% 11.9M 15s
88100K .......... .......... .......... .......... .......... 33% 12.0M 15s
88150K .......... .......... .......... .......... .......... 33% 12.6M 15s
88200K .......... .......... .......... .......... .......... 33% 24.1M 15s
88250K .......... .......... .......... .......... .......... 33% 12.8M 15s
88300K .......... .......... .......... .......... .......... 33% 12.4M 15s
88350K .......... .......... .......... .......... .......... 33% 12.3M 15s
88400K .......... .......... .......... .......... .......... 33% 10.9M 14s
88450K .......... .......... .......... .......... .......... 33% 12.6M 14s
88500K .......... .......... .......... .......... .......... 33% 11.8M 14s
88550K .......... .......... .......... .......... .......... 33% 6.09M 14s
88600K .......... .......... .......... .......... .......... 33% 16.7M 14s
88650K .......... .......... .......... .......... .......... 33% 35.7M 14s
88700K .......... .......... .......... .......... .......... 33% 11.0M 14s
88750K .......... .......... .......... .......... .......... 33% 11.2M 14s
88800K .......... .......... .......... .......... .......... 33% 12.2M 14s
88850K .......... .......... .......... .......... .......... 33% 7.74M 14s
88900K .......... .......... .......... .......... .......... 33% 10.5M 14s
88950K .......... .......... .......... .......... .......... 33% 11.7M 14s
89000K .......... .......... .......... .......... .......... 33% 11.4M 14s
89050K .......... .......... .......... .......... .......... 33% 12.8M 14s
89100K .......... .......... .......... .......... .......... 33% 11.4M 14s
89150K .......... .......... .......... .......... .......... 33% 19.0M 14s
89200K .......... .......... .......... .......... .......... 33% 6.81M 14s
89250K .......... .......... .......... .......... .......... 33% 13.0M 14s
89300K .......... .......... .......... .......... .......... 33% 12.5M 14s
89350K .......... .......... .......... .......... .......... 33% 9.79M 14s
89400K .......... .......... .......... .......... .......... 33% 13.1M 14s
89450K .......... .......... .......... .......... .......... 33% 11.5M 14s
89500K .......... .......... .......... .......... .......... 33% 12.8M 14s
89550K .......... .......... .......... .......... .......... 33% 12.1M 14s
89600K .......... .......... .......... .......... .......... 33% 11.5M 14s
89650K .......... .......... .......... .......... .......... 33% 12.7M 14s
89700K .......... .......... .......... .......... .......... 33% 10.6M 14s
89750K .......... .......... .......... .......... .......... 33% 12.5M 14s
89800K .......... .......... .......... .......... .......... 33% 15.4M 14s
89850K .......... .......... .......... .......... .......... 33% 10.0M 14s
89900K .......... .......... .......... .......... .......... 33% 16.4M 14s
89950K .......... .......... .......... .......... .......... 33% 12.7M 14s
90000K .......... .......... .......... .......... .......... 33% 25.8M 14s
90050K .......... .......... .......... .......... .......... 33% 14.0M 14s
90100K .......... .......... .......... .......... .......... 33% 12.3M 14s
90150K .......... .......... .......... .......... .......... 33% 12.1M 14s
90200K .......... .......... .......... .......... .......... 33% 14.3M 14s
90250K .......... .......... .......... .......... .......... 34% 13.6M 14s
90300K .......... .......... .......... .......... .......... 34% 16.6M 14s
90350K .......... .......... .......... .......... .......... 34% 12.5M 14s
90400K .......... .......... .......... .......... .......... 34% 11.8M 14s
90450K .......... .......... .......... .......... .......... 34% 12.8M 14s
90500K .......... .......... .......... .......... .......... 34% 9.75M 14s
90550K .......... .......... .......... .......... .......... 34% 18.3M 14s
90600K .......... .......... .......... .......... .......... 34% 18.4M 14s
90650K .......... .......... .......... .......... .......... 34% 11.9M 14s
90700K .......... .......... .......... .......... .......... 34% 13.2M 14s
90750K .......... .......... .......... .......... .......... 34% 17.1M 14s
90800K .......... .......... .......... .......... .......... 34% 20.7M 14s
90850K .......... .......... .......... .......... .......... 34% 10.2M 14s
90900K .......... .......... .......... .......... .......... 34% 12.1M 14s
90950K .......... .......... .......... .......... .......... 34% 12.1M 14s
91000K .......... .......... .......... .......... .......... 34% 15.1M 14s
91050K .......... .......... .......... .......... .......... 34% 34.2M 14s
91100K .......... .......... .......... .......... .......... 34% 11.8M 14s
91150K .......... .......... .......... .......... .......... 34% 12.1M 14s
91200K .......... .......... .......... .......... .......... 34% 10.7M 14s
91250K .......... .......... .......... .......... .......... 34% 74.6M 14s
91300K .......... .......... .......... .......... .......... 34% 14.2M 14s
91350K .......... .......... .......... .......... .......... 34% 11.5M 14s
91400K .......... .......... .......... .......... .......... 34% 5.46M 14s
91450K .......... .......... .......... .......... .......... 34% 48.0M 14s
91500K .......... .......... .......... .......... .......... 34% 98.2M 14s
91550K .......... .......... .......... .......... .......... 34% 8.83M 14s
91600K .......... .......... .......... .......... .......... 34% 10.4M 14s
91650K .......... .......... .......... .......... .......... 34% 12.2M 14s
91700K .......... .......... .......... .......... .......... 34% 10.2M 14s
91750K .......... .......... .......... .......... .......... 34% 13.7M 14s
91800K .......... .......... .......... .......... .......... 34% 14.8M 14s
91850K .......... .......... .......... .......... .......... 34% 10.5M 14s
91900K .......... .......... .......... .......... .......... 34% 19.5M 14s
91950K .......... .......... .......... .......... .......... 34% 11.7M 14s
92000K .......... .......... .......... .......... .......... 34% 12.1M 14s
92050K .......... .......... .......... .......... .......... 34% 12.4M 14s
92100K .......... .......... .......... .......... .......... 34% 11.9M 14s
92150K .......... .......... .......... .......... .......... 34% 14.4M 14s
92200K .......... .......... .......... .......... .......... 34% 10.4M 14s
92250K .......... .......... .......... .......... .......... 34% 12.8M 14s
92300K .......... .......... .......... .......... .......... 34% 12.9M 14s
92350K .......... .......... .......... .......... .......... 34% 6.37M 14s
92400K .......... .......... .......... .......... .......... 34% 65.9M 14s
92450K .......... .......... .......... .......... .......... 34% 7.35M 14s
92500K .......... .......... .......... .......... .......... 34% 9.16M 14s
92550K .......... .......... .......... .......... .......... 34% 11.9M 14s
92600K .......... .......... .......... .......... .......... 34% 7.78M 14s
92650K .......... .......... .......... .......... .......... 34% 8.14M 14s
92700K .......... .......... .......... .......... .......... 34% 11.9M 14s
92750K .......... .......... .......... .......... .......... 34% 11.9M 14s
92800K .......... .......... .......... .......... .......... 34% 12.2M 14s
92850K .......... .......... .......... .......... .......... 34% 6.58M 14s
92900K .......... .......... .......... .......... .......... 35% 11.0M 14s
92950K .......... .......... .......... .......... .......... 35% 4.18M 14s
93000K .......... .......... .......... .......... .......... 35% 26.3M 14s
93050K .......... .......... .......... .......... .......... 35% 101M 14s
93100K .......... .......... .......... .......... .......... 35% 6.64M 14s
93150K .......... .......... .......... .......... .......... 35% 6.37M 14s
93200K .......... .......... .......... .......... .......... 35% 9.65M 14s
93250K .......... .......... .......... .......... .......... 35% 6.20M 14s
93300K .......... .......... .......... .......... .......... 35% 10.6M 14s
93350K .......... .......... .......... .......... .......... 35% 5.71M 14s
93400K .......... .......... .......... .......... .......... 35% 11.2M 14s
93450K .......... .......... .......... .......... .......... 35% 6.25M 14s
93500K .......... .......... .......... .......... .......... 35% 12.1M 14s
93550K .......... .......... .......... .......... .......... 35% 10.1M 14s
93600K .......... .......... .......... .......... .......... 35% 6.69M 14s
93650K .......... .......... .......... .......... .......... 35% 10.3M 14s
93700K .......... .......... .......... .......... .......... 35% 10.1M 14s
93750K .......... .......... .......... .......... .......... 35% 12.7M 14s
93800K .......... .......... .......... .......... .......... 35% 12.4M 14s
93850K .......... .......... .......... .......... .......... 35% 7.75M 14s
93900K .......... .......... .......... .......... .......... 35% 8.50M 14s
93950K .......... .......... .......... .......... .......... 35% 12.2M 14s
94000K .......... .......... .......... .......... .......... 35% 11.8M 14s
94050K .......... .......... .......... .......... .......... 35% 12.2M 14s
94100K .......... .......... .......... .......... .......... 35% 9.54M 14s
94150K .......... .......... .......... .......... .......... 35% 10.7M 14s
94200K .......... .......... .......... .......... .......... 35% 7.73M 14s
94250K .......... .......... .......... .......... .......... 35% 25.0M 14s
94300K .......... .......... .......... .......... .......... 35% 12.0M 14s
94350K .......... .......... .......... .......... .......... 35% 12.1M 14s
94400K .......... .......... .......... .......... .......... 35% 7.47M 14s
94450K .......... .......... .......... .......... .......... 35% 12.5M 14s
94500K .......... .......... .......... .......... .......... 35% 13.4M 14s
94550K .......... .......... .......... .......... .......... 35% 19.1M 14s
94600K .......... .......... .......... .......... .......... 35% 14.7M 14s
94650K .......... .......... .......... .......... .......... 35% 13.4M 14s
94700K .......... .......... .......... .......... .......... 35% 11.3M 14s
94750K .......... .......... .......... .......... .......... 35% 11.3M 14s
94800K .......... .......... .......... .......... .......... 35% 12.4M 14s
94850K .......... .......... .......... .......... .......... 35% 12.5M 14s
94900K .......... .......... .......... .......... .......... 35% 12.0M 14s
94950K .......... .......... .......... .......... .......... 35% 13.7M 14s
95000K .......... .......... .......... .......... .......... 35% 13.4M 14s
95050K .......... .......... .......... .......... .......... 35% 11.3M 14s
95100K .......... .......... .......... .......... .......... 35% 15.6M 14s
95150K .......... .......... .......... .......... .......... 35% 11.9M 14s
95200K .......... .......... .......... .......... .......... 35% 13.3M 14s
95250K .......... .......... .......... .......... .......... 35% 13.0M 14s
95300K .......... .......... .......... .......... .......... 35% 28.4M 14s
95350K .......... .......... .......... .......... .......... 35% 11.8M 14s
95400K .......... .......... .......... .......... .......... 35% 12.9M 14s
95450K .......... .......... .......... .......... .......... 35% 12.9M 14s
95500K .......... .......... .......... .......... .......... 35% 16.0M 14s
95550K .......... .......... .......... .......... .......... 36% 22.1M 14s
95600K .......... .......... .......... .......... .......... 36% 4.22M 14s
95650K .......... .......... .......... .......... .......... 36% 55.3M 14s
95700K .......... .......... .......... .......... .......... 36% 185M 14s
95750K .......... .......... .......... .......... .......... 36% 11.3M 14s
95800K .......... .......... .......... .......... .......... 36% 12.3M 14s
95850K .......... .......... .......... .......... .......... 36% 9.20M 14s
95900K .......... .......... .......... .......... .......... 36% 10.3M 14s
95950K .......... .......... .......... .......... .......... 36% 6.24M 14s
96000K .......... .......... .......... .......... .......... 36% 10.3M 14s
96050K .......... .......... .......... .......... .......... 36% 11.5M 14s
96100K .......... .......... .......... .......... .......... 36% 12.3M 14s
96150K .......... .......... .......... .......... .......... 36% 9.04M 14s
96200K .......... .......... .......... .......... .......... 36% 8.99M 14s
96250K .......... .......... .......... .......... .......... 36% 14.2M 14s
96300K .......... .......... .......... .......... .......... 36% 9.98M 14s
96350K .......... .......... .......... .......... .......... 36% 11.7M 14s
96400K .......... .......... .......... .......... .......... 36% 9.61M 14s
96450K .......... .......... .......... .......... .......... 36% 10.4M 14s
96500K .......... .......... .......... .......... .......... 36% 9.31M 14s
96550K .......... .......... .......... .......... .......... 36% 9.60M 14s
96600K .......... .......... .......... .......... .......... 36% 18.0M 14s
96650K .......... .......... .......... .......... .......... 36% 11.3M 14s
96700K .......... .......... .......... .......... .......... 36% 12.8M 14s
96750K .......... .......... .......... .......... .......... 36% 13.6M 14s
96800K .......... .......... .......... .......... .......... 36% 11.0M 14s
96850K .......... .......... .......... .......... .......... 36% 11.1M 14s
96900K .......... .......... .......... .......... .......... 36% 21.4M 14s
96950K .......... .......... .......... .......... .......... 36% 7.60M 14s
97000K .......... .......... .......... .......... .......... 36% 23.0M 14s
97050K .......... .......... .......... .......... .......... 36% 11.7M 14s
97100K .......... .......... .......... .......... .......... 36% 11.8M 14s
97150K .......... .......... .......... .......... .......... 36% 13.1M 14s
97200K .......... .......... .......... .......... .......... 36% 20.0M 14s
97250K .......... .......... .......... .......... .......... 36% 15.5M 14s
97300K .......... .......... .......... .......... .......... 36% 13.3M 14s
97350K .......... .......... .......... .......... .......... 36% 11.7M 14s
97400K .......... .......... .......... .......... .......... 36% 21.9M 14s
97450K .......... .......... .......... .......... .......... 36% 14.1M 14s
97500K .......... .......... .......... .......... .......... 36% 11.8M 14s
97550K .......... .......... .......... .......... .......... 36% 14.2M 14s
97600K .......... .......... .......... .......... .......... 36% 13.6M 14s
97650K .......... .......... .......... .......... .......... 36% 15.4M 14s
97700K .......... .......... .......... .......... .......... 36% 17.4M 14s
97750K .......... .......... .......... .......... .......... 36% 18.0M 14s
97800K .......... .......... .......... .......... .......... 36% 13.6M 14s
97850K .......... .......... .......... .......... .......... 36% 16.3M 14s
97900K .......... .......... .......... .......... .......... 36% 29.0M 14s
97950K .......... .......... .......... .......... .......... 36% 12.1M 14s
98000K .......... .......... .......... .......... .......... 36% 12.4M 14s
98050K .......... .......... .......... .......... .......... 36% 17.3M 14s
98100K .......... .......... .......... .......... .......... 36% 16.1M 14s
98150K .......... .......... .......... .......... .......... 36% 19.5M 14s
98200K .......... .......... .......... .......... .......... 37% 12.4M 14s
98250K .......... .......... .......... .......... .......... 37% 22.0M 14s
98300K .......... .......... .......... .......... .......... 37% 12.8M 14s
98350K .......... .......... .......... .......... .......... 37% 4.53M 14s
98400K .......... .......... .......... .......... .......... 37% 89.3M 14s
98450K .......... .......... .......... .......... .......... 37% 58.9M 14s
98500K .......... .......... .......... .......... .......... 37% 16.9M 14s
98550K .......... .......... .......... .......... .......... 37% 13.3M 14s
98600K .......... .......... .......... .......... .......... 37% 7.14M 14s
98650K .......... .......... .......... .......... .......... 37% 41.2M 14s
98700K .......... .......... .......... .......... .......... 37% 6.61M 14s
98750K .......... .......... .......... .......... .......... 37% 12.5M 14s
98800K .......... .......... .......... .......... .......... 37% 9.51M 14s
98850K .......... .......... .......... .......... .......... 37% 8.27M 14s
98900K .......... .......... .......... .......... .......... 37% 10.7M 14s
98950K .......... .......... .......... .......... .......... 37% 7.33M 14s
99000K .......... .......... .......... .......... .......... 37% 10.2M 14s
99050K .......... .......... .......... .......... .......... 37% 9.91M 14s
99100K .......... .......... .......... .......... .......... 37% 7.21M 14s
99150K .......... .......... .......... .......... .......... 37% 9.54M 14s
99200K .......... .......... .......... .......... .......... 37% 9.06M 14s
99250K .......... .......... .......... .......... .......... 37% 11.5M 14s
99300K .......... .......... .......... .......... .......... 37% 13.7M 14s
99350K .......... .......... .......... .......... .......... 37% 11.2M 14s
99400K .......... .......... .......... .......... .......... 37% 9.71M 14s
99450K .......... .......... .......... .......... .......... 37% 9.33M 14s
99500K .......... .......... .......... .......... .......... 37% 19.0M 14s
99550K .......... .......... .......... .......... .......... 37% 11.4M 14s
99600K .......... .......... .......... .......... .......... 37% 9.47M 14s
99650K .......... .......... .......... .......... .......... 37% 8.71M 14s
99700K .......... .......... .......... .......... .......... 37% 11.5M 14s
99750K .......... .......... .......... .......... .......... 37% 10.6M 14s
99800K .......... .......... .......... .......... .......... 37% 11.0M 14s
99850K .......... .......... .......... .......... .......... 37% 11.5M 14s
99900K .......... .......... .......... .......... .......... 37% 11.6M 14s
99950K .......... .......... .......... .......... .......... 37% 11.5M 14s
100000K .......... .......... .......... .......... .......... 37% 13.5M 14s
100050K .......... .......... .......... .......... .......... 37% 20.8M 14s
100100K .......... .......... .......... .......... .......... 37% 11.1M 14s
100150K .......... .......... .......... .......... .......... 37% 11.6M 14s
100200K .......... .......... .......... .......... .......... 37% 12.3M 14s
100250K .......... .......... .......... .......... .......... 37% 12.3M 14s
100300K .......... .......... .......... .......... .......... 37% 10.1M 14s
100350K .......... .......... .......... .......... .......... 37% 10.8M 14s
100400K .......... .......... .......... .......... .......... 37% 14.0M 14s
100450K .......... .......... .......... .......... .......... 37% 19.2M 14s
100500K .......... .......... .......... .......... .......... 37% 12.4M 14s
100550K .......... .......... .......... .......... .......... 37% 29.0M 14s
100600K .......... .......... .......... .......... .......... 37% 13.1M 14s
100650K .......... .......... .......... .......... .......... 37% 12.3M 14s
100700K .......... .......... .......... .......... .......... 37% 13.1M 14s
100750K .......... .......... .......... .......... .......... 37% 37.0M 14s
100800K .......... .......... .......... .......... .......... 37% 15.0M 14s
100850K .......... .......... .......... .......... .......... 38% 11.3M 14s
100900K .......... .......... .......... .......... .......... 38% 12.1M 14s
100950K .......... .......... .......... .......... .......... 38% 11.1M 13s
101000K .......... .......... .......... .......... .......... 38% 45.4M 13s
101050K .......... .......... .......... .......... .......... 38% 10.7M 13s
101100K .......... .......... .......... .......... .......... 38% 14.2M 13s
101150K .......... .......... .......... .......... .......... 38% 19.1M 13s
101200K .......... .......... .......... .......... .......... 38% 16.3M 13s
101250K .......... .......... .......... .......... .......... 38% 17.1M 13s
101300K .......... .......... .......... .......... .......... 38% 11.8M 13s
101350K .......... .......... .......... .......... .......... 38% 97.7M 13s
101400K .......... .......... .......... .......... .......... 38% 12.2M 13s
101450K .......... .......... .......... .......... .......... 38% 10.2M 13s
101500K .......... .......... .......... .......... .......... 38% 15.8M 13s
101550K .......... .......... .......... .......... .......... 38% 53.2M 13s
101600K .......... .......... .......... .......... .......... 38% 11.7M 13s
101650K .......... .......... .......... .......... .......... 38% 72.5M 13s
101700K .......... .......... .......... .......... .......... 38% 11.7M 13s
101750K .......... .......... .......... .......... .......... 38% 14.3M 13s
101800K .......... .......... .......... .......... .......... 38% 17.0M 13s
101850K .......... .......... .......... .......... .......... 38% 34.7M 13s
101900K .......... .......... .......... .......... .......... 38% 11.1M 13s
101950K .......... .......... .......... .......... .......... 38% 11.6M 13s
102000K .......... .......... .......... .......... .......... 38% 101M 13s
102050K .......... .......... .......... .......... .......... 38% 13.0M 13s
102100K .......... .......... .......... .......... .......... 38% 12.9M 13s
102150K .......... .......... .......... .......... .......... 38% 34.9M 13s
102200K .......... .......... .......... .......... .......... 38% 12.2M 13s
102250K .......... .......... .......... .......... .......... 38% 19.5M 13s
102300K .......... .......... .......... .......... .......... 38% 6.01M 13s
102350K .......... .......... .......... .......... .......... 38% 58.2M 13s
102400K .......... .......... .......... .......... .......... 38% 31.6M 13s
102450K .......... .......... .......... .......... .......... 38% 14.6M 13s
102500K .......... .......... .......... .......... .......... 38% 13.0M 13s
102550K .......... .......... .......... .......... .......... 38% 10.6M 13s
102600K .......... .......... .......... .......... .......... 38% 11.3M 13s
102650K .......... .......... .......... .......... .......... 38% 14.5M 13s
102700K .......... .......... .......... .......... .......... 38% 10.8M 13s
102750K .......... .......... .......... .......... .......... 38% 12.6M 13s
102800K .......... .......... .......... .......... .......... 38% 14.3M 13s
102850K .......... .......... .......... .......... .......... 38% 10.7M 13s
102900K .......... .......... .......... .......... .......... 38% 12.3M 13s
102950K .......... .......... .......... .......... .......... 38% 11.7M 13s
103000K .......... .......... .......... .......... .......... 38% 12.8M 13s
103050K .......... .......... .......... .......... .......... 38% 14.6M 13s
103100K .......... .......... .......... .......... .......... 38% 11.7M 13s
103150K .......... .......... .......... .......... .......... 38% 14.7M 13s
103200K .......... .......... .......... .......... .......... 38% 12.5M 13s
103250K .......... .......... .......... .......... .......... 38% 12.7M 13s
103300K .......... .......... .......... .......... .......... 38% 19.6M 13s
103350K .......... .......... .......... .......... .......... 38% 19.1M 13s
103400K .......... .......... .......... .......... .......... 38% 12.4M 13s
103450K .......... .......... .......... .......... .......... 38% 11.9M 13s
103500K .......... .......... .......... .......... .......... 39% 13.1M 13s
103550K .......... .......... .......... .......... .......... 39% 20.0M 13s
103600K .......... .......... .......... .......... .......... 39% 17.8M 13s
103650K .......... .......... .......... .......... .......... 39% 11.0M 13s
103700K .......... .......... .......... .......... .......... 39% 9.91M 13s
103750K .......... .......... .......... .......... .......... 39% 17.1M 13s
103800K .......... .......... .......... .......... .......... 39% 23.2M 13s
103850K .......... .......... .......... .......... .......... 39% 14.7M 13s
103900K .......... .......... .......... .......... .......... 39% 10.7M 13s
103950K .......... .......... .......... .......... .......... 39% 11.2M 13s
104000K .......... .......... .......... .......... .......... 39% 21.9M 13s
104050K .......... .......... .......... .......... .......... 39% 13.5M 13s
104100K .......... .......... .......... .......... .......... 39% 9.17M 13s
104150K .......... .......... .......... .......... .......... 39% 18.4M 13s
104200K .......... .......... .......... .......... .......... 39% 11.5M 13s
104250K .......... .......... .......... .......... .......... 39% 14.7M 13s
104300K .......... .......... .......... .......... .......... 39% 28.4M 13s
104350K .......... .......... .......... .......... .......... 39% 11.4M 13s
104400K .......... .......... .......... .......... .......... 39% 14.6M 13s
104450K .......... .......... .......... .......... .......... 39% 12.2M 13s
104500K .......... .......... .......... .......... .......... 39% 11.8M 13s
104550K .......... .......... .......... .......... .......... 39% 4.49M 13s
104600K .......... .......... .......... .......... .......... 39% 89.1M 13s
104650K .......... .......... .......... .......... .......... 39% 86.2M 13s
104700K .......... .......... .......... .......... .......... 39% 11.3M 13s
104750K .......... .......... .......... .......... .......... 39% 15.0M 13s
104800K .......... .......... .......... .......... .......... 39% 15.2M 13s
104850K .......... .......... .......... .......... .......... 39% 13.7M 13s
104900K .......... .......... .......... .......... .......... 39% 11.8M 13s
104950K .......... .......... .......... .......... .......... 39% 6.71M 13s
105000K .......... .......... .......... .......... .......... 39% 11.5M 13s
105050K .......... .......... .......... .......... .......... 39% 10.3M 13s
105100K .......... .......... .......... .......... .......... 39% 11.9M 13s
105150K .......... .......... .......... .......... .......... 39% 12.5M 13s
105200K .......... .......... .......... .......... .......... 39% 8.94M 13s
105250K .......... .......... .......... .......... .......... 39% 24.3M 13s
105300K .......... .......... .......... .......... .......... 39% 12.2M 13s
105350K .......... .......... .......... .......... .......... 39% 8.98M 13s
105400K .......... .......... .......... .......... .......... 39% 11.0M 13s
105450K .......... .......... .......... .......... .......... 39% 10.0M 13s
105500K .......... .......... .......... .......... .......... 39% 15.4M 13s
105550K .......... .......... .......... .......... .......... 39% 9.72M 13s
105600K .......... .......... .......... .......... .......... 39% 9.04M 13s
105650K .......... .......... .......... .......... .......... 39% 11.9M 13s
105700K .......... .......... .......... .......... .......... 39% 9.56M 13s
105750K .......... .......... .......... .......... .......... 39% 24.4M 13s
105800K .......... .......... .......... .......... .......... 39% 11.8M 13s
105850K .......... .......... .......... .......... .......... 39% 9.61M 13s
105900K .......... .......... .......... .......... .......... 39% 10.4M 13s
105950K .......... .......... .......... .......... .......... 39% 9.85M 13s
106000K .......... .......... .......... .......... .......... 39% 21.7M 13s
106050K .......... .......... .......... .......... .......... 39% 11.2M 13s
106100K .......... .......... .......... .......... .......... 39% 11.8M 13s
106150K .......... .......... .......... .......... .......... 39% 15.4M 13s
106200K .......... .......... .......... .......... .......... 40% 11.4M 13s
106250K .......... .......... .......... .......... .......... 40% 12.5M 13s
106300K .......... .......... .......... .......... .......... 40% 14.0M 13s
106350K .......... .......... .......... .......... .......... 40% 14.2M 13s
106400K .......... .......... .......... .......... .......... 40% 26.2M 13s
106450K .......... .......... .......... .......... .......... 40% 14.4M 13s
106500K .......... .......... .......... .......... .......... 40% 6.47M 13s
106550K .......... .......... .......... .......... .......... 40% 123M 13s
106600K .......... .......... .......... .......... .......... 40% 15.6M 13s
106650K .......... .......... .......... .......... .......... 40% 12.5M 13s
106700K .......... .......... .......... .......... .......... 40% 15.8M 13s
106750K .......... .......... .......... .......... .......... 40% 13.5M 13s
106800K .......... .......... .......... .......... .......... 40% 15.2M 13s
106850K .......... .......... .......... .......... .......... 40% 12.9M 13s
106900K .......... .......... .......... .......... .......... 40% 15.9M 13s
106950K .......... .......... .......... .......... .......... 40% 11.1M 13s
107000K .......... .......... .......... .......... .......... 40% 15.5M 13s
107050K .......... .......... .......... .......... .......... 40% 15.5M 13s
107100K .......... .......... .......... .......... .......... 40% 13.2M 13s
107150K .......... .......... .......... .......... .......... 40% 12.3M 13s
107200K .......... .......... .......... .......... .......... 40% 10.5M 13s
107250K .......... .......... .......... .......... .......... 40% 19.2M 13s
107300K .......... .......... .......... .......... .......... 40% 12.0M 13s
107350K .......... .......... .......... .......... .......... 40% 10.4M 13s
107400K .......... .......... .......... .......... .......... 40% 17.1M 13s
107450K .......... .......... .......... .......... .......... 40% 11.7M 13s
107500K .......... .......... .......... .......... .......... 40% 12.7M 13s
107550K .......... .......... .......... .......... .......... 40% 13.0M 13s
107600K .......... .......... .......... .......... .......... 40% 12.5M 13s
107650K .......... .......... .......... .......... .......... 40% 15.5M 13s
107700K .......... .......... .......... .......... .......... 40% 13.3M 13s
107750K .......... .......... .......... .......... .......... 40% 12.4M 13s
107800K .......... .......... .......... .......... .......... 40% 16.9M 13s
107850K .......... .......... .......... .......... .......... 40% 21.2M 13s
107900K .......... .......... .......... .......... .......... 40% 13.3M 13s
107950K .......... .......... .......... .......... .......... 40% 12.0M 13s
108000K .......... .......... .......... .......... .......... 40% 12.2M 13s
108050K .......... .......... .......... .......... .......... 40% 14.2M 13s
108100K .......... .......... .......... .......... .......... 40% 15.4M 13s
108150K .......... .......... .......... .......... .......... 40% 24.7M 13s
108200K .......... .......... .......... .......... .......... 40% 12.5M 13s
108250K .......... .......... .......... .......... .......... 40% 16.5M 13s
108300K .......... .......... .......... .......... .......... 40% 36.9M 13s
108350K .......... .......... .......... .......... .......... 40% 12.7M 13s
108400K .......... .......... .......... .......... .......... 40% 12.8M 13s
108450K .......... .......... .......... .......... .......... 40% 11.6M 13s
108500K .......... .......... .......... .......... .......... 40% 19.2M 13s
108550K .......... .......... .......... .......... .......... 40% 29.0M 13s
108600K .......... .......... .......... .......... .......... 40% 6.18M 13s
108650K .......... .......... .......... .......... .......... 40% 85.3M 13s
108700K .......... .......... .......... .......... .......... 40% 14.5M 13s
108750K .......... .......... .......... .......... .......... 40% 12.3M 13s
108800K .......... .......... .......... .......... .......... 40% 11.8M 13s
108850K .......... .......... .......... .......... .......... 41% 13.6M 13s
108900K .......... .......... .......... .......... .......... 41% 12.6M 13s
108950K .......... .......... .......... .......... .......... 41% 12.9M 13s
109000K .......... .......... .......... .......... .......... 41% 11.6M 13s
109050K .......... .......... .......... .......... .......... 41% 11.7M 13s
109100K .......... .......... .......... .......... .......... 41% 12.3M 13s
109150K .......... .......... .......... .......... .......... 41% 12.2M 13s
109200K .......... .......... .......... .......... .......... 41% 7.92M 13s
109250K .......... .......... .......... .......... .......... 41% 11.8M 13s
109300K .......... .......... .......... .......... .......... 41% 19.9M 13s
109350K .......... .......... .......... .......... .......... 41% 10.2M 13s
109400K .......... .......... .......... .......... .......... 41% 14.0M 13s
109450K .......... .......... .......... .......... .......... 41% 13.2M 13s
109500K .......... .......... .......... .......... .......... 41% 13.0M 13s
109550K .......... .......... .......... .......... .......... 41% 10.6M 13s
109600K .......... .......... .......... .......... .......... 41% 12.9M 13s
109650K .......... .......... .......... .......... .......... 41% 11.8M 13s
109700K .......... .......... .......... .......... .......... 41% 11.1M 13s
109750K .......... .......... .......... .......... .......... 41% 40.2M 13s
109800K .......... .......... .......... .......... .......... 41% 12.8M 13s
109850K .......... .......... .......... .......... .......... 41% 11.0M 13s
109900K .......... .......... .......... .......... .......... 41% 12.3M 13s
109950K .......... .......... .......... .......... .......... 41% 10.7M 13s
110000K .......... .......... .......... .......... .......... 41% 12.1M 13s
110050K .......... .......... .......... .......... .......... 41% 10.9M 13s
110100K .......... .......... .......... .......... .......... 41% 20.8M 13s
110150K .......... .......... .......... .......... .......... 41% 12.4M 13s
110200K .......... .......... .......... .......... .......... 41% 6.83M 13s
110250K .......... .......... .......... .......... .......... 41% 6.52M 13s
110300K .......... .......... .......... .......... .......... 41% 88.9M 13s
110350K .......... .......... .......... .......... .......... 41% 12.0M 13s
110400K .......... .......... .......... .......... .......... 41% 9.73M 13s
110450K .......... .......... .......... .......... .......... 41% 6.56M 13s
110500K .......... .......... .......... .......... .......... 41% 8.32M 13s
110550K .......... .......... .......... .......... .......... 41% 11.5M 13s
110600K .......... .......... .......... .......... .......... 41% 5.99M 13s
110650K .......... .......... .......... .......... .......... 41% 8.20M 13s
110700K .......... .......... .......... .......... .......... 41% 8.65M 13s
110750K .......... .......... .......... .......... .......... 41% 8.05M 13s
110800K .......... .......... .......... .......... .......... 41% 9.30M 13s
110850K .......... .......... .......... .......... .......... 41% 11.7M 13s
110900K .......... .......... .......... .......... .......... 41% 8.69M 13s
110950K .......... .......... .......... .......... .......... 41% 7.87M 13s
111000K .......... .......... .......... .......... .......... 41% 12.4M 13s
111050K .......... .......... .......... .......... .......... 41% 12.1M 13s
111100K .......... .......... .......... .......... .......... 41% 7.33M 13s
111150K .......... .......... .......... .......... .......... 41% 13.5M 13s
111200K .......... .......... .......... .......... .......... 41% 10.1M 13s
111250K .......... .......... .......... .......... .......... 41% 11.3M 13s
111300K .......... .......... .......... .......... .......... 41% 11.7M 13s
111350K .......... .......... .......... .......... .......... 41% 9.05M 13s
111400K .......... .......... .......... .......... .......... 41% 11.3M 13s
111450K .......... .......... .......... .......... .......... 41% 4.47M 13s
111500K .......... .......... .......... .......... .......... 42% 72.5M 13s
111550K .......... .......... .......... .......... .......... 42% 33.1M 13s
111600K .......... .......... .......... .......... .......... 42% 10.8M 13s
111650K .......... .......... .......... .......... .......... 42% 7.41M 13s
111700K .......... .......... .......... .......... .......... 42% 10.9M 13s
111750K .......... .......... .......... .......... .......... 42% 6.98M 13s
111800K .......... .......... .......... .......... .......... 42% 11.9M 13s
111850K .......... .......... .......... .......... .......... 42% 8.15M 13s
111900K .......... .......... .......... .......... .......... 42% 9.87M 13s
111950K .......... .......... .......... .......... .......... 42% 9.34M 13s
112000K .......... .......... .......... .......... .......... 42% 13.8M 13s
112050K .......... .......... .......... .......... .......... 42% 7.56M 13s
112100K .......... .......... .......... .......... .......... 42% 8.98M 13s
112150K .......... .......... .......... .......... .......... 42% 9.89M 13s
112200K .......... .......... .......... .......... .......... 42% 10.6M 13s
112250K .......... .......... .......... .......... .......... 42% 7.73M 13s
112300K .......... .......... .......... .......... .......... 42% 11.5M 13s
112350K .......... .......... .......... .......... .......... 42% 9.76M 13s
112400K .......... .......... .......... .......... .......... 42% 11.5M 13s
112450K .......... .......... .......... .......... .......... 42% 10.2M 13s
112500K .......... .......... .......... .......... .......... 42% 12.6M 12s
112550K .......... .......... .......... .......... .......... 42% 11.1M 12s
112600K .......... .......... .......... .......... .......... 42% 11.3M 12s
112650K .......... .......... .......... .......... .......... 42% 11.0M 12s
112700K .......... .......... .......... .......... .......... 42% 10.7M 12s
112750K .......... .......... .......... .......... .......... 42% 10.4M 12s
112800K .......... .......... .......... .......... .......... 42% 11.2M 12s
112850K .......... .......... .......... .......... .......... 42% 11.2M 12s
112900K .......... .......... .......... .......... .......... 42% 5.47M 12s
112950K .......... .......... .......... .......... .......... 42% 46.0M 12s
113000K .......... .......... .......... .......... .......... 42% 7.73M 12s
113050K .......... .......... .......... .......... .......... 42% 11.5M 12s
113100K .......... .......... .......... .......... .......... 42% 6.94M 12s
113150K .......... .......... .......... .......... .......... 42% 9.66M 12s
113200K .......... .......... .......... .......... .......... 42% 7.16M 12s
113250K .......... .......... .......... .......... .......... 42% 8.72M 12s
113300K .......... .......... .......... .......... .......... 42% 7.26M 12s
113350K .......... .......... .......... .......... .......... 42% 5.77M 12s
113400K .......... .......... .......... .......... .......... 42% 9.79M 12s
113450K .......... .......... .......... .......... .......... 42% 6.19M 12s
113500K .......... .......... .......... .......... .......... 42% 6.32M 12s
113550K .......... .......... .......... .......... .......... 42% 5.77M 12s
113600K .......... .......... .......... .......... .......... 42% 9.86M 12s
113650K .......... .......... .......... .......... .......... 42% 6.49M 12s
113700K .......... .......... .......... .......... .......... 42% 5.88M 12s
113750K .......... .......... .......... .......... .......... 42% 9.83M 12s
113800K .......... .......... .......... .......... .......... 42% 9.78M 12s
113850K .......... .......... .......... .......... .......... 42% 5.22M 12s
113900K .......... .......... .......... .......... .......... 42% 5.01M 12s
113950K .......... .......... .......... .......... .......... 42% 6.96M 12s
114000K .......... .......... .......... .......... .......... 42% 7.96M 12s
114050K .......... .......... .......... .......... .......... 42% 8.01M 12s
114100K .......... .......... .......... .......... .......... 42% 10.1M 12s
114150K .......... .......... .......... .......... .......... 43% 8.17M 12s
114200K .......... .......... .......... .......... .......... 43% 7.77M 12s
114250K .......... .......... .......... .......... .......... 43% 6.92M 12s
114300K .......... .......... .......... .......... .......... 43% 10.9M 12s
114350K .......... .......... .......... .......... .......... 43% 11.5M 12s
114400K .......... .......... .......... .......... .......... 43% 7.24M 12s
114450K .......... .......... .......... .......... .......... 43% 9.62M 12s
114500K .......... .......... .......... .......... .......... 43% 5.83M 12s
114550K .......... .......... .......... .......... .......... 43% 6.59M 12s
114600K .......... .......... .......... .......... .......... 43% 6.01M 12s
114650K .......... .......... .......... .......... .......... 43% 6.96M 12s
114700K .......... .......... .......... .......... .......... 43% 6.54M 12s
114750K .......... .......... .......... .......... .......... 43% 8.76M 12s
114800K .......... .......... .......... .......... .......... 43% 9.09M 12s
114850K .......... .......... .......... .......... .......... 43% 7.07M 12s
114900K .......... .......... .......... .......... .......... 43% 7.57M 12s
114950K .......... .......... .......... .......... .......... 43% 7.19M 12s
115000K .......... .......... .......... .......... .......... 43% 8.25M 12s
115050K .......... .......... .......... .......... .......... 43% 10.6M 12s
115100K .......... .......... .......... .......... .......... 43% 12.4M 12s
115150K .......... .......... .......... .......... .......... 43% 8.94M 12s
115200K .......... .......... .......... .......... .......... 43% 9.66M 12s
115250K .......... .......... .......... .......... .......... 43% 7.86M 12s
115300K .......... .......... .......... .......... .......... 43% 10.6M 12s
115350K .......... .......... .......... .......... .......... 43% 11.7M 12s
115400K .......... .......... .......... .......... .......... 43% 13.6M 12s
115450K .......... .......... .......... .......... .......... 43% 7.26M 12s
115500K .......... .......... .......... .......... .......... 43% 12.5M 12s
115550K .......... .......... .......... .......... .......... 43% 13.8M 12s
115600K .......... .......... .......... .......... .......... 43% 10.4M 12s
115650K .......... .......... .......... .......... .......... 43% 14.3M 12s
115700K .......... .......... .......... .......... .......... 43% 12.6M 12s
115750K .......... .......... .......... .......... .......... 43% 12.6M 12s
115800K .......... .......... .......... .......... .......... 43% 14.9M 12s
115850K .......... .......... .......... .......... .......... 43% 10.2M 12s
115900K .......... .......... .......... .......... .......... 43% 22.0M 12s
115950K .......... .......... .......... .......... .......... 43% 11.5M 12s
116000K .......... .......... .......... .......... .......... 43% 16.5M 12s
116050K .......... .......... .......... .......... .......... 43% 15.1M 12s
116100K .......... .......... .......... .......... .......... 43% 12.3M 12s
116150K .......... .......... .......... .......... .......... 43% 16.7M 12s
116200K .......... .......... .......... .......... .......... 43% 12.3M 12s
116250K .......... .......... .......... .......... .......... 43% 10.8M 12s
116300K .......... .......... .......... .......... .......... 43% 14.9M 12s
116350K .......... .......... .......... .......... .......... 43% 18.3M 12s
116400K .......... .......... .......... .......... .......... 43% 29.1M 12s
116450K .......... .......... .......... .......... .......... 43% 13.3M 12s
116500K .......... .......... .......... .......... .......... 43% 12.0M 12s
116550K .......... .......... .......... .......... .......... 43% 23.1M 12s
116600K .......... .......... .......... .......... .......... 43% 14.7M 12s
116650K .......... .......... .......... .......... .......... 43% 15.9M 12s
116700K .......... .......... .......... .......... .......... 43% 13.2M 12s
116750K .......... .......... .......... .......... .......... 43% 23.7M 12s
116800K .......... .......... .......... .......... .......... 44% 31.6M 12s
116850K .......... .......... .......... .......... .......... 44% 10.5M 12s
116900K .......... .......... .......... .......... .......... 44% 22.6M 12s
116950K .......... .......... .......... .......... .......... 44% 14.1M 12s
117000K .......... .......... .......... .......... .......... 44% 11.2M 12s
117050K .......... .......... .......... .......... .......... 44% 109M 12s
117100K .......... .......... .......... .......... .......... 44% 14.5M 12s
117150K .......... .......... .......... .......... .......... 44% 17.0M 12s
117200K .......... .......... .......... .......... .......... 44% 15.2M 12s
117250K .......... .......... .......... .......... .......... 44% 8.06M 12s
117300K .......... .......... .......... .......... .......... 44% 14.0M 12s
117350K .......... .......... .......... .......... .......... 44% 80.5M 12s
117400K .......... .......... .......... .......... .......... 44% 12.4M 12s
117450K .......... .......... .......... .......... .......... 44% 10.6M 12s
117500K .......... .......... .......... .......... .......... 44% 14.6M 12s
117550K .......... .......... .......... .......... .......... 44% 12.8M 12s
117600K .......... .......... .......... .......... .......... 44% 6.35M 12s
117650K .......... .......... .......... .......... .......... 44% 9.88M 12s
117700K .......... .......... .......... .......... .......... 44% 9.46M 12s
117750K .......... .......... .......... .......... .......... 44% 7.48M 12s
117800K .......... .......... .......... .......... .......... 44% 8.09M 12s
117850K .......... .......... .......... .......... .......... 44% 8.52M 12s
117900K .......... .......... .......... .......... .......... 44% 8.86M 12s
117950K .......... .......... .......... .......... .......... 44% 7.18M 12s
118000K .......... .......... .......... .......... .......... 44% 9.60M 12s
118050K .......... .......... .......... .......... .......... 44% 7.75M 12s
118100K .......... .......... .......... .......... .......... 44% 4.62M 12s
118150K .......... .......... .......... .......... .......... 44% 25.2M 12s
118200K .......... .......... .......... .......... .......... 44% 7.04M 12s
118250K .......... .......... .......... .......... .......... 44% 5.43M 12s
118300K .......... .......... .......... .......... .......... 44% 4.30M 12s
118350K .......... .......... .......... .......... .......... 44% 4.34M 12s
118400K .......... .......... .......... .......... .......... 44% 5.36M 12s
118450K .......... .......... .......... .......... .......... 44% 3.86M 12s
118500K .......... .......... .......... .......... .......... 44% 5.03M 12s
118550K .......... .......... .......... .......... .......... 44% 4.74M 12s
118600K .......... .......... .......... .......... .......... 44% 5.16M 12s
118650K .......... .......... .......... .......... .......... 44% 4.47M 12s
118700K .......... .......... .......... .......... .......... 44% 4.50M 12s
118750K .......... .......... .......... .......... .......... 44% 3.68M 12s
118800K .......... .......... .......... .......... .......... 44% 6.26M 12s
118850K .......... .......... .......... .......... .......... 44% 4.65M 12s
118900K .......... .......... .......... .......... .......... 44% 12.5M 12s
118950K .......... .......... .......... .......... .......... 44% 5.04M 12s
119000K .......... .......... .......... .......... .......... 44% 11.9M 12s
119050K .......... .......... .......... .......... .......... 44% 8.28M 12s
119100K .......... .......... .......... .......... .......... 44% 7.92M 12s
119150K .......... .......... .......... .......... .......... 44% 6.29M 12s
119200K .......... .......... .......... .......... .......... 44% 15.8M 12s
119250K .......... .......... .......... .......... .......... 44% 9.57M 12s
119300K .......... .......... .......... .......... .......... 44% 9.90M 12s
119350K .......... .......... .......... .......... .......... 44% 9.27M 12s
119400K .......... .......... .......... .......... .......... 44% 9.28M 12s
119450K .......... .......... .......... .......... .......... 45% 8.07M 12s
119500K .......... .......... .......... .......... .......... 45% 6.86M 12s
119550K .......... .......... .......... .......... .......... 45% 10.6M 12s
119600K .......... .......... .......... .......... .......... 45% 8.14M 12s
119650K .......... .......... .......... .......... .......... 45% 10.8M 12s
119700K .......... .......... .......... .......... .......... 45% 7.84M 12s
119750K .......... .......... .......... .......... .......... 45% 10.9M 12s
119800K .......... .......... .......... .......... .......... 45% 11.4M 12s
119850K .......... .......... .......... .......... .......... 45% 7.53M 12s
119900K .......... .......... .......... .......... .......... 45% 8.69M 12s
119950K .......... .......... .......... .......... .......... 45% 8.07M 12s
120000K .......... .......... .......... .......... .......... 45% 14.9M 12s
120050K .......... .......... .......... .......... .......... 45% 9.74M 12s
120100K .......... .......... .......... .......... .......... 45% 8.08M 12s
120150K .......... .......... .......... .......... .......... 45% 8.71M 12s
120200K .......... .......... .......... .......... .......... 45% 8.90M 12s
120250K .......... .......... .......... .......... .......... 45% 11.2M 12s
120300K .......... .......... .......... .......... .......... 45% 7.96M 12s
120350K .......... .......... .......... .......... .......... 45% 11.1M 12s
120400K .......... .......... .......... .......... .......... 45% 8.45M 12s
120450K .......... .......... .......... .......... .......... 45% 9.32M 12s
120500K .......... .......... .......... .......... .......... 45% 8.43M 12s
120550K .......... .......... .......... .......... .......... 45% 10.1M 12s
120600K .......... .......... .......... .......... .......... 45% 8.79M 12s
120650K .......... .......... .......... .......... .......... 45% 10.3M 12s
120700K .......... .......... .......... .......... .......... 45% 9.19M 12s
120750K .......... .......... .......... .......... .......... 45% 9.96M 12s
120800K .......... .......... .......... .......... .......... 45% 10.3M 12s
120850K .......... .......... .......... .......... .......... 45% 9.05M 12s
120900K .......... .......... .......... .......... .......... 45% 11.0M 12s
120950K .......... .......... .......... .......... .......... 45% 11.2M 12s
121000K .......... .......... .......... .......... .......... 45% 10.1M 12s
121050K .......... .......... .......... .......... .......... 45% 12.4M 12s
121100K .......... .......... .......... .......... .......... 45% 12.1M 12s
121150K .......... .......... .......... .......... .......... 45% 13.4M 12s
121200K .......... .......... .......... .......... .......... 45% 11.6M 12s
121250K .......... .......... .......... .......... .......... 45% 12.4M 12s
121300K .......... .......... .......... .......... .......... 45% 11.2M 12s
121350K .......... .......... .......... .......... .......... 45% 10.1M 12s
121400K .......... .......... .......... .......... .......... 45% 12.8M 12s
121450K .......... .......... .......... .......... .......... 45% 12.1M 12s
121500K .......... .......... .......... .......... .......... 45% 16.8M 12s
121550K .......... .......... .......... .......... .......... 45% 12.2M 12s
121600K .......... .......... .......... .......... .......... 45% 10.7M 12s
121650K .......... .......... .......... .......... .......... 45% 11.2M 12s
121700K .......... .......... .......... .......... .......... 45% 17.7M 12s
121750K .......... .......... .......... .......... .......... 45% 18.7M 12s
121800K .......... .......... .......... .......... .......... 45% 4.56M 12s
121850K .......... .......... .......... .......... .......... 45% 175M 12s
121900K .......... .......... .......... .......... .......... 45% 23.2M 12s
121950K .......... .......... .......... .......... .......... 45% 6.61M 12s
122000K .......... .......... .......... .......... .......... 45% 12.3M 12s
122050K .......... .......... .......... .......... .......... 45% 10.6M 12s
122100K .......... .......... .......... .......... .......... 46% 10.7M 12s
122150K .......... .......... .......... .......... .......... 46% 10.8M 12s
122200K .......... .......... .......... .......... .......... 46% 10.3M 12s
122250K .......... .......... .......... .......... .......... 46% 11.7M 12s
122300K .......... .......... .......... .......... .......... 46% 11.0M 12s
122350K .......... .......... .......... .......... .......... 46% 10.8M 12s
122400K .......... .......... .......... .......... .......... 46% 12.3M 12s
122450K .......... .......... .......... .......... .......... 46% 9.58M 12s
122500K .......... .......... .......... .......... .......... 46% 10.8M 12s
122550K .......... .......... .......... .......... .......... 46% 10.5M 12s
122600K .......... .......... .......... .......... .......... 46% 8.24M 12s
122650K .......... .......... .......... .......... .......... 46% 13.6M 12s
122700K .......... .......... .......... .......... .......... 46% 14.8M 12s
122750K .......... .......... .......... .......... .......... 46% 11.0M 12s
122800K .......... .......... .......... .......... .......... 46% 11.3M 12s
122850K .......... .......... .......... .......... .......... 46% 11.9M 12s
122900K .......... .......... .......... .......... .......... 46% 11.3M 12s
122950K .......... .......... .......... .......... .......... 46% 10.4M 12s
123000K .......... .......... .......... .......... .......... 46% 11.5M 12s
123050K .......... .......... .......... .......... .......... 46% 11.4M 12s
123100K .......... .......... .......... .......... .......... 46% 9.85M 12s
123150K .......... .......... .......... .......... .......... 46% 11.7M 12s
123200K .......... .......... .......... .......... .......... 46% 11.5M 12s
123250K .......... .......... .......... .......... .......... 46% 22.1M 12s
123300K .......... .......... .......... .......... .......... 46% 10.7M 12s
123350K .......... .......... .......... .......... .......... 46% 10.5M 12s
123400K .......... .......... .......... .......... .......... 46% 11.3M 12s
123450K .......... .......... .......... .......... .......... 46% 7.18M 12s
123500K .......... .......... .......... .......... .......... 46% 16.0M 12s
123550K .......... .......... .......... .......... .......... 46% 9.10M 12s
123600K .......... .......... .......... .......... .......... 46% 8.57M 12s
123650K .......... .......... .......... .......... .......... 46% 10.9M 12s
123700K .......... .......... .......... .......... .......... 46% 10.2M 12s
123750K .......... .......... .......... .......... .......... 46% 9.81M 12s
123800K .......... .......... .......... .......... .......... 46% 8.54M 12s
123850K .......... .......... .......... .......... .......... 46% 10.5M 12s
123900K .......... .......... .......... .......... .......... 46% 6.90M 12s
123950K .......... .......... .......... .......... .......... 46% 13.9M 12s
124000K .......... .......... .......... .......... .......... 46% 13.5M 12s
124050K .......... .......... .......... .......... .......... 46% 11.7M 12s
124100K .......... .......... .......... .......... .......... 46% 6.03M 12s
124150K .......... .......... .......... .......... .......... 46% 9.07M 12s
124200K .......... .......... .......... .......... .......... 46% 10.9M 12s
124250K .......... .......... .......... .......... .......... 46% 11.9M 12s
124300K .......... .......... .......... .......... .......... 46% 5.19M 12s
124350K .......... .......... .......... .......... .......... 46% 31.7M 12s
124400K .......... .......... .......... .......... .......... 46% 8.74M 12s
124450K .......... .......... .......... .......... .......... 46% 6.50M 12s
124500K .......... .......... .......... .......... .......... 46% 7.68M 12s
124550K .......... .......... .......... .......... .......... 46% 7.75M 12s
124600K .......... .......... .......... .......... .......... 46% 7.13M 12s
124650K .......... .......... .......... .......... .......... 46% 3.88M 12s
124700K .......... .......... .......... .......... .......... 46% 40.0M 12s
124750K .......... .......... .......... .......... .......... 47% 7.33M 12s
124800K .......... .......... .......... .......... .......... 47% 6.66M 12s
124850K .......... .......... .......... .......... .......... 47% 6.08M 12s
124900K .......... .......... .......... .......... .......... 47% 5.92M 12s
124950K .......... .......... .......... .......... .......... 47% 11.3M 12s
125000K .......... .......... .......... .......... .......... 47% 6.93M 12s
125050K .......... .......... .......... .......... .......... 47% 10.8M 12s
125100K .......... .......... .......... .......... .......... 47% 7.00M 12s
125150K .......... .......... .......... .......... .......... 47% 12.1M 12s
125200K .......... .......... .......... .......... .......... 47% 6.45M 12s
125250K .......... .......... .......... .......... .......... 47% 12.5M 12s
125300K .......... .......... .......... .......... .......... 47% 11.1M 12s
125350K .......... .......... .......... .......... .......... 47% 5.85M 12s
125400K .......... .......... .......... .......... .......... 47% 10.2M 12s
125450K .......... .......... .......... .......... .......... 47% 10.0M 12s
125500K .......... .......... .......... .......... .......... 47% 7.17M 12s
125550K .......... .......... .......... .......... .......... 47% 9.63M 12s
125600K .......... .......... .......... .......... .......... 47% 10.9M 12s
125650K .......... .......... .......... .......... .......... 47% 9.80M 12s
125700K .......... .......... .......... .......... .......... 47% 7.45M 12s
125750K .......... .......... .......... .......... .......... 47% 11.8M 12s
125800K .......... .......... .......... .......... .......... 47% 11.3M 12s
125850K .......... .......... .......... .......... .......... 47% 11.1M 12s
125900K .......... .......... .......... .......... .......... 47% 11.9M 12s
125950K .......... .......... .......... .......... .......... 47% 11.4M 12s
126000K .......... .......... .......... .......... .......... 47% 10.5M 12s
126050K .......... .......... .......... .......... .......... 47% 11.9M 12s
126100K .......... .......... .......... .......... .......... 47% 14.2M 12s
126150K .......... .......... .......... .......... .......... 47% 11.7M 12s
126200K .......... .......... .......... .......... .......... 47% 11.2M 12s
126250K .......... .......... .......... .......... .......... 47% 11.7M 12s
126300K .......... .......... .......... .......... .......... 47% 18.8M 12s
126350K .......... .......... .......... .......... .......... 47% 10.3M 12s
126400K .......... .......... .......... .......... .......... 47% 45.4M 12s
126450K .......... .......... .......... .......... .......... 47% 8.80M 12s
126500K .......... .......... .......... .......... .......... 47% 12.2M 12s
126550K .......... .......... .......... .......... .......... 47% 26.2M 12s
126600K .......... .......... .......... .......... .......... 47% 11.7M 12s
126650K .......... .......... .......... .......... .......... 47% 12.1M 12s
126700K .......... .......... .......... .......... .......... 47% 15.2M 12s
126750K .......... .......... .......... .......... .......... 47% 10.5M 12s
126800K .......... .......... .......... .......... .......... 47% 17.8M 12s
126850K .......... .......... .......... .......... .......... 47% 14.7M 12s
126900K .......... .......... .......... .......... .......... 47% 26.2M 12s
126950K .......... .......... .......... .......... .......... 47% 12.0M 12s
127000K .......... .......... .......... .......... .......... 47% 11.0M 12s
127050K .......... .......... .......... .......... .......... 47% 13.2M 12s
127100K .......... .......... .......... .......... .......... 47% 9.23M 12s
127150K .......... .......... .......... .......... .......... 47% 14.7M 12s
127200K .......... .......... .......... .......... .......... 47% 12.4M 12s
127250K .......... .......... .......... .......... .......... 47% 29.8M 12s
127300K .......... .......... .......... .......... .......... 47% 12.7M 12s
127350K .......... .......... .......... .......... .......... 47% 8.18M 12s
127400K .......... .......... .......... .......... .......... 48% 22.8M 12s
127450K .......... .......... .......... .......... .......... 48% 12.1M 12s
127500K .......... .......... .......... .......... .......... 48% 11.5M 12s
127550K .......... .......... .......... .......... .......... 48% 11.5M 12s
127600K .......... .......... .......... .......... .......... 48% 8.08M 12s
127650K .......... .......... .......... .......... .......... 48% 9.13M 12s
127700K .......... .......... .......... .......... .......... 48% 11.6M 12s
127750K .......... .......... .......... .......... .......... 48% 11.8M 12s
127800K .......... .......... .......... .......... .......... 48% 7.84M 12s
127850K .......... .......... .......... .......... .......... 48% 11.4M 12s
127900K .......... .......... .......... .......... .......... 48% 5.33M 12s
127950K .......... .......... .......... .......... .......... 48% 41.2M 12s
128000K .......... .......... .......... .......... .......... 48% 8.24M 12s
128050K .......... .......... .......... .......... .......... 48% 11.7M 12s
128100K .......... .......... .......... .......... .......... 48% 10.1M 12s
128150K .......... .......... .......... .......... .......... 48% 7.40M 12s
128200K .......... .......... .......... .......... .......... 48% 10.7M 12s
128250K .......... .......... .......... .......... .......... 48% 8.62M 12s
128300K .......... .......... .......... .......... .......... 48% 6.54M 12s
128350K .......... .......... .......... .......... .......... 48% 20.2M 12s
128400K .......... .......... .......... .......... .......... 48% 8.50M 12s
128450K .......... .......... .......... .......... .......... 48% 8.94M 12s
128500K .......... .......... .......... .......... .......... 48% 7.33M 12s
128550K .......... .......... .......... .......... .......... 48% 9.00M 12s
128600K .......... .......... .......... .......... .......... 48% 8.20M 12s
128650K .......... .......... .......... .......... .......... 48% 6.37M 12s
128700K .......... .......... .......... .......... .......... 48% 8.40M 12s
128750K .......... .......... .......... .......... .......... 48% 7.54M 12s
128800K .......... .......... .......... .......... .......... 48% 7.21M 12s
128850K .......... .......... .......... .......... .......... 48% 10.8M 12s
128900K .......... .......... .......... .......... .......... 48% 8.32M 12s
128950K .......... .......... .......... .......... .......... 48% 5.91M 12s
129000K .......... .......... .......... .......... .......... 48% 12.6M 12s
129050K .......... .......... .......... .......... .......... 48% 11.3M 12s
129100K .......... .......... .......... .......... .......... 48% 9.64M 12s
129150K .......... .......... .......... .......... .......... 48% 11.8M 12s
129200K .......... .......... .......... .......... .......... 48% 6.77M 12s
129250K .......... .......... .......... .......... .......... 48% 12.0M 12s
129300K .......... .......... .......... .......... .......... 48% 12.2M 12s
129350K .......... .......... .......... .......... .......... 48% 10.4M 12s
129400K .......... .......... .......... .......... .......... 48% 12.2M 12s
129450K .......... .......... .......... .......... .......... 48% 6.19M 12s
129500K .......... .......... .......... .......... .......... 48% 19.7M 11s
129550K .......... .......... .......... .......... .......... 48% 12.9M 11s
129600K .......... .......... .......... .......... .......... 48% 6.32M 11s
129650K .......... .......... .......... .......... .......... 48% 11.0M 11s
129700K .......... .......... .......... .......... .......... 48% 8.14M 11s
129750K .......... .......... .......... .......... .......... 48% 10.1M 11s
129800K .......... .......... .......... .......... .......... 48% 12.1M 11s
129850K .......... .......... .......... .......... .......... 48% 8.10M 11s
129900K .......... .......... .......... .......... .......... 48% 13.1M 11s
129950K .......... .......... .......... .......... .......... 48% 8.71M 11s
130000K .......... .......... .......... .......... .......... 48% 10.5M 11s
130050K .......... .......... .......... .......... .......... 49% 12.4M 11s
130100K .......... .......... .......... .......... .......... 49% 12.7M 11s
130150K .......... .......... .......... .......... .......... 49% 8.74M 11s
130200K .......... .......... .......... .......... .......... 49% 10.2M 11s
130250K .......... .......... .......... .......... .......... 49% 13.5M 11s
130300K .......... .......... .......... .......... .......... 49% 12.0M 11s
130350K .......... .......... .......... .......... .......... 49% 9.25M 11s
130400K .......... .......... .......... .......... .......... 49% 9.87M 11s
130450K .......... .......... .......... .......... .......... 49% 13.0M 11s
130500K .......... .......... .......... .......... .......... 49% 12.1M 11s
130550K .......... .......... .......... .......... .......... 49% 12.8M 11s
130600K .......... .......... .......... .......... .......... 49% 9.18M 11s
130650K .......... .......... .......... .......... .......... 49% 13.9M 11s
130700K .......... .......... .......... .......... .......... 49% 10.2M 11s
130750K .......... .......... .......... .......... .......... 49% 19.2M 11s
130800K .......... .......... .......... .......... .......... 49% 12.7M 11s
130850K .......... .......... .......... .......... .......... 49% 12.7M 11s
130900K .......... .......... .......... .......... .......... 49% 9.73M 11s
130950K .......... .......... .......... .......... .......... 49% 12.6M 11s
131000K .......... .......... .......... .......... .......... 49% 13.7M 11s
131050K .......... .......... .......... .......... .......... 49% 12.7M 11s
131100K .......... .......... .......... .......... .......... 49% 11.6M 11s
131150K .......... .......... .......... .......... .......... 49% 14.4M 11s
131200K .......... .......... .......... .......... .......... 49% 12.7M 11s
131250K .......... .......... .......... .......... .......... 49% 11.9M 11s
131300K .......... .......... .......... .......... .......... 49% 11.7M 11s
131350K .......... .......... .......... .......... .......... 49% 12.0M 11s
131400K .......... .......... .......... .......... .......... 49% 18.2M 11s
131450K .......... .......... .......... .......... .......... 49% 4.95M 11s
131500K .......... .......... .......... .......... .......... 49% 25.8M 11s
131550K .......... .......... .......... .......... .......... 49% 18.5M 11s
131600K .......... .......... .......... .......... .......... 49% 8.52M 11s
131650K .......... .......... .......... .......... .......... 49% 10.5M 11s
131700K .......... .......... .......... .......... .......... 49% 11.9M 11s
131750K .......... .......... .......... .......... .......... 49% 8.85M 11s
131800K .......... .......... .......... .......... .......... 49% 9.68M 11s
131850K .......... .......... .......... .......... .......... 49% 10.9M 11s
131900K .......... .......... .......... .......... .......... 49% 9.68M 11s
131950K .......... .......... .......... .......... .......... 49% 10.8M 11s
132000K .......... .......... .......... .......... .......... 49% 12.6M 11s
132050K .......... .......... .......... .......... .......... 49% 13.0M 11s
132100K .......... .......... .......... .......... .......... 49% 11.7M 11s
132150K .......... .......... .......... .......... .......... 49% 12.4M 11s
132200K .......... .......... .......... .......... .......... 49% 10.8M 11s
132250K .......... .......... .......... .......... .......... 49% 8.33M 11s
132300K .......... .......... .......... .......... .......... 49% 12.6M 11s
132350K .......... .......... .......... .......... .......... 49% 8.20M 11s
132400K .......... .......... .......... .......... .......... 49% 12.0M 11s
132450K .......... .......... .......... .......... .......... 49% 12.7M 11s
132500K .......... .......... .......... .......... .......... 49% 10.5M 11s
132550K .......... .......... .......... .......... .......... 49% 12.8M 11s
132600K .......... .......... .......... .......... .......... 49% 14.0M 11s
132650K .......... .......... .......... .......... .......... 49% 13.5M 11s
132700K .......... .......... .......... .......... .......... 49% 14.3M 11s
132750K .......... .......... .......... .......... .......... 50% 15.4M 11s
132800K .......... .......... .......... .......... .......... 50% 16.1M 11s
132850K .......... .......... .......... .......... .......... 50% 15.7M 11s
132900K .......... .......... .......... .......... .......... 50% 15.0M 11s
132950K .......... .......... .......... .......... .......... 50% 20.3M 11s
133000K .......... .......... .......... .......... .......... 50% 16.8M 11s
133050K .......... .......... .......... .......... .......... 50% 22.7M 11s
133100K .......... .......... .......... .......... .......... 50% 12.7M 11s
133150K .......... .......... .......... .......... .......... 50% 34.5M 11s
133200K .......... .......... .......... .......... .......... 50% 15.1M 11s
133250K .......... .......... .......... .......... .......... 50% 16.0M 11s
133300K .......... .......... .......... .......... .......... 50% 14.4M 11s
133350K .......... .......... .......... .......... .......... 50% 17.3M 11s
133400K .......... .......... .......... .......... .......... 50% 26.2M 11s
133450K .......... .......... .......... .......... .......... 50% 14.0M 11s
133500K .......... .......... .......... .......... .......... 50% 13.5M 11s
133550K .......... .......... .......... .......... .......... 50% 17.3M 11s
133600K .......... .......... .......... .......... .......... 50% 17.7M 11s
133650K .......... .......... .......... .......... .......... 50% 22.9M 11s
133700K .......... .......... .......... .......... .......... 50% 7.70M 11s
133750K .......... .......... .......... .......... .......... 50% 36.4M 11s
133800K .......... .......... .......... .......... .......... 50% 19.1M 11s
133850K .......... .......... .......... .......... .......... 50% 16.0M 11s
133900K .......... .......... .......... .......... .......... 50% 18.5M 11s
133950K .......... .......... .......... .......... .......... 50% 12.6M 11s
134000K .......... .......... .......... .......... .......... 50% 14.6M 11s
134050K .......... .......... .......... .......... .......... 50% 21.9M 11s
134100K .......... .......... .......... .......... .......... 50% 8.35M 11s
134150K .......... .......... .......... .......... .......... 50% 9.33M 11s
134200K .......... .......... .......... .......... .......... 50% 17.7M 11s
134250K .......... .......... .......... .......... .......... 50% 11.9M 11s
134300K .......... .......... .......... .......... .......... 50% 48.6M 11s
134350K .......... .......... .......... .......... .......... 50% 155M 11s
134400K .......... .......... .......... .......... .......... 50% 23.8M 11s
134450K .......... .......... .......... .......... .......... 50% 26.2M 11s
134500K .......... .......... .......... .......... .......... 50% 18.0M 11s
134550K .......... .......... .......... .......... .......... 50% 15.6M 11s
134600K .......... .......... .......... .......... .......... 50% 19.3M 11s
134650K .......... .......... .......... .......... .......... 50% 20.9M 11s
134700K .......... .......... .......... .......... .......... 50% 14.3M 11s
134750K .......... .......... .......... .......... .......... 50% 19.2M 11s
134800K .......... .......... .......... .......... .......... 50% 19.9M 11s
134850K .......... .......... .......... .......... .......... 50% 18.9M 11s
134900K .......... .......... .......... .......... .......... 50% 15.9M 11s
134950K .......... .......... .......... .......... .......... 50% 23.0M 11s
135000K .......... .......... .......... .......... .......... 50% 14.4M 11s
135050K .......... .......... .......... .......... .......... 50% 22.0M 11s
135100K .......... .......... .......... .......... .......... 50% 17.4M 11s
135150K .......... .......... .......... .......... .......... 50% 3.45M 11s
135200K .......... .......... .......... .......... .......... 50% 39.2M 11s
135250K .......... .......... .......... .......... .......... 50% 258M 11s
135300K .......... .......... .......... .......... .......... 50% 156M 11s
135350K .......... .......... .......... .......... .......... 50% 10.7M 11s
135400K .......... .......... .......... .......... .......... 51% 38.0M 11s
135450K .......... .......... .......... .......... .......... 51% 18.0M 11s
135500K .......... .......... .......... .......... .......... 51% 10.7M 11s
135550K .......... .......... .......... .......... .......... 51% 12.9M 11s
135600K .......... .......... .......... .......... .......... 51% 13.2M 11s
135650K .......... .......... .......... .......... .......... 51% 7.34M 11s
135700K .......... .......... .......... .......... .......... 51% 13.4M 11s
135750K .......... .......... .......... .......... .......... 51% 12.8M 11s
135800K .......... .......... .......... .......... .......... 51% 7.62M 11s
135850K .......... .......... .......... .......... .......... 51% 9.84M 11s
135900K .......... .......... .......... .......... .......... 51% 12.3M 11s
135950K .......... .......... .......... .......... .......... 51% 10.5M 11s
136000K .......... .......... .......... .......... .......... 51% 13.7M 11s
136050K .......... .......... .......... .......... .......... 51% 7.53M 11s
136100K .......... .......... .......... .......... .......... 51% 10.5M 11s
136150K .......... .......... .......... .......... .......... 51% 7.82M 11s
136200K .......... .......... .......... .......... .......... 51% 4.71M 11s
136250K .......... .......... .......... .......... .......... 51% 6.51M 11s
136300K .......... .......... .......... .......... .......... 51% 5.20M 11s
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136450K .......... .......... .......... .......... .......... 51% 6.42M 11s
136500K .......... .......... .......... .......... .......... 51% 5.31M 11s
136550K .......... .......... .......... .......... .......... 51% 7.57M 11s
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136700K .......... .......... .......... .......... .......... 51% 6.20M 11s
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136800K .......... .......... .......... .......... .......... 51% 8.83M 11s
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136900K .......... .......... .......... .......... .......... 51% 6.67M 11s
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137000K .......... .......... .......... .......... .......... 51% 4.01M 11s
137050K .......... .......... .......... .......... .......... 51% 25.1M 11s
137100K .......... .......... .......... .......... .......... 51% 4.36M 11s
137150K .......... .......... .......... .......... .......... 51% 4.89M 11s
137200K .......... .......... .......... .......... .......... 51% 5.31M 11s
137250K .......... .......... .......... .......... .......... 51% 6.49M 11s
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137700K .......... .......... .......... .......... .......... 51% 5.07M 11s
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137900K .......... .......... .......... .......... .......... 51% 7.51M 11s
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138000K .......... .......... .......... .......... .......... 51% 9.75M 11s
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138100K .......... .......... .......... .......... .......... 52% 11.1M 11s
138150K .......... .......... .......... .......... .......... 52% 10.4M 11s
138200K .......... .......... .......... .......... .......... 52% 7.40M 11s
138250K .......... .......... .......... .......... .......... 52% 13.0M 11s
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138350K .......... .......... .......... .......... .......... 52% 8.06M 11s
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138850K .......... .......... .......... .......... .......... 52% 9.75M 11s
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139000K .......... .......... .......... .......... .......... 52% 9.49M 11s
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139100K .......... .......... .......... .......... .......... 52% 8.55M 11s
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139200K .......... .......... .......... .......... .......... 52% 8.81M 11s
139250K .......... .......... .......... .......... .......... 52% 13.6M 11s
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140000K .......... .......... .......... .......... .......... 52% 11.5M 11s
140050K .......... .......... .......... .......... .......... 52% 19.3M 11s
140100K .......... .......... .......... .......... .......... 52% 11.4M 11s
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140200K .......... .......... .......... .......... .......... 52% 10.2M 11s
140250K .......... .......... .......... .......... .......... 52% 6.81M 11s
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142150K .......... .......... .......... .......... .......... 53% 6.44M 11s
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142500K .......... .......... .......... .......... .......... 53% 9.89M 11s
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142700K .......... .......... .......... .......... .......... 53% 7.48M 11s
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142800K .......... .......... .......... .......... .......... 53% 12.6M 11s
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142950K .......... .......... .......... .......... .......... 53% 7.44M 11s
143000K .......... .......... .......... .......... .......... 53% 10.3M 11s
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143100K .......... .......... .......... .......... .......... 53% 9.00M 11s
143150K .......... .......... .......... .......... .......... 53% 9.18M 11s
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143250K .......... .......... .......... .......... .......... 53% 9.01M 11s
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143550K .......... .......... .......... .......... .......... 54% 27.3M 11s
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144250K .......... .......... .......... .......... .......... 54% 6.12M 11s
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144350K .......... .......... .......... .......... .......... 54% 5.76M 11s
144400K .......... .......... .......... .......... .......... 54% 6.06M 10s
144450K .......... .......... .......... .......... .......... 54% 7.39M 10s
144500K .......... .......... .......... .......... .......... 54% 7.06M 10s
144550K .......... .......... .......... .......... .......... 54% 5.66M 10s
144600K .......... .......... .......... .......... .......... 54% 6.09M 10s
144650K .......... .......... .......... .......... .......... 54% 8.47M 10s
144700K .......... .......... .......... .......... .......... 54% 3.98M 10s
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144800K .......... .......... .......... .......... .......... 54% 6.72M 10s
144850K .......... .......... .......... .......... .......... 54% 4.31M 10s
144900K .......... .......... .......... .......... .......... 54% 6.42M 10s
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145000K .......... .......... .......... .......... .......... 54% 8.00M 10s
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145100K .......... .......... .......... .......... .......... 54% 5.06M 10s
145150K .......... .......... .......... .......... .......... 54% 7.57M 10s
145200K .......... .......... .......... .......... .......... 54% 5.66M 10s
145250K .......... .......... .......... .......... .......... 54% 8.79M 10s
145300K .......... .......... .......... .......... .......... 54% 5.63M 10s
145350K .......... .......... .......... .......... .......... 54% 7.20M 10s
145400K .......... .......... .......... .......... .......... 54% 6.15M 10s
145450K .......... .......... .......... .......... .......... 54% 5.31M 10s
145500K .......... .......... .......... .......... .......... 54% 9.06M 10s
145550K .......... .......... .......... .......... .......... 54% 7.57M 10s
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146000K .......... .......... .......... .......... .......... 55% 10.2M 10s
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146100K .......... .......... .......... .......... .......... 55% 8.53M 10s
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146200K .......... .......... .......... .......... .......... 55% 9.98M 10s
146250K .......... .......... .......... .......... .......... 55% 14.7M 10s
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146900K .......... .......... .......... .......... .......... 55% 6.49M 10s
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147000K .......... .......... .......... .......... .......... 55% 11.3M 10s
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147100K .......... .......... .......... .......... .......... 55% 6.29M 10s
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149000K .......... .......... .......... .......... .......... 56% 10.5M 10s
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158150K .......... .......... .......... .......... .......... 59% 37.3M 9s
158200K .......... .......... .......... .......... .......... 59% 12.1M 9s
158250K .......... .......... .......... .......... .......... 59% 12.4M 9s
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158500K .......... .......... .......... .......... .......... 59% 110M 9s
158550K .......... .......... .......... .......... .......... 59% 17.9M 9s
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158700K .......... .......... .......... .......... .......... 59% 11.5M 9s
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158800K .......... .......... .......... .......... .......... 59% 15.7M 9s
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158900K .......... .......... .......... .......... .......... 59% 9.48M 9s
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159250K .......... .......... .......... .......... .......... 59% 7.40M 9s
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159550K .......... .......... .......... .......... .......... 60% 11.5M 9s
159600K .......... .......... .......... .......... .......... 60% 11.2M 9s
159650K .......... .......... .......... .......... .......... 60% 12.7M 9s
159700K .......... .......... .......... .......... .......... 60% 11.1M 9s
159750K .......... .......... .......... .......... .......... 60% 10.5M 9s
159800K .......... .......... .......... .......... .......... 60% 12.2M 9s
159850K .......... .......... .......... .......... .......... 60% 7.40M 9s
159900K .......... .......... .......... .......... .......... 60% 11.7M 9s
159950K .......... .......... .......... .......... .......... 60% 10.6M 9s
160000K .......... .......... .......... .......... .......... 60% 20.9M 9s
160050K .......... .......... .......... .......... .......... 60% 13.0M 9s
160100K .......... .......... .......... .......... .......... 60% 6.20M 9s
160150K .......... .......... .......... .......... .......... 60% 41.9M 9s
160200K .......... .......... .......... .......... .......... 60% 6.72M 9s
160250K .......... .......... .......... .......... .......... 60% 9.26M 9s
160300K .......... .......... .......... .......... .......... 60% 11.0M 9s
160350K .......... .......... .......... .......... .......... 60% 5.80M 9s
160400K .......... .......... .......... .......... .......... 60% 11.1M 9s
160450K .......... .......... .......... .......... .......... 60% 10.2M 9s
160500K .......... .......... .......... .......... .......... 60% 8.79M 9s
160550K .......... .......... .......... .......... .......... 60% 10.1M 9s
160600K .......... .......... .......... .......... .......... 60% 10.9M 9s
160650K .......... .......... .......... .......... .......... 60% 12.9M 9s
160700K .......... .......... .......... .......... .......... 60% 12.4M 9s
160750K .......... .......... .......... .......... .......... 60% 8.47M 9s
160800K .......... .......... .......... .......... .......... 60% 9.38M 9s
160850K .......... .......... .......... .......... .......... 60% 9.92M 9s
160900K .......... .......... .......... .......... .......... 60% 12.9M 9s
160950K .......... .......... .......... .......... .......... 60% 10.2M 9s
161000K .......... .......... .......... .......... .......... 60% 12.1M 9s
161050K .......... .......... .......... .......... .......... 60% 11.7M 9s
161100K .......... .......... .......... .......... .......... 60% 11.2M 9s
161150K .......... .......... .......... .......... .......... 60% 9.89M 9s
161200K .......... .......... .......... .......... .......... 60% 5.53M 9s
161250K .......... .......... .......... .......... .......... 60% 67.9M 9s
161300K .......... .......... .......... .......... .......... 60% 7.58M 9s
161350K .......... .......... .......... .......... .......... 60% 9.69M 9s
161400K .......... .......... .......... .......... .......... 60% 7.20M 9s
161450K .......... .......... .......... .......... .......... 60% 10.7M 9s
161500K .......... .......... .......... .......... .......... 60% 7.99M 9s
161550K .......... .......... .......... .......... .......... 60% 9.03M 9s
161600K .......... .......... .......... .......... .......... 60% 10.4M 9s
161650K .......... .......... .......... .......... .......... 60% 8.42M 9s
161700K .......... .......... .......... .......... .......... 60% 8.67M 9s
161750K .......... .......... .......... .......... .......... 60% 10.6M 9s
161800K .......... .......... .......... .......... .......... 60% 7.93M 9s
161850K .......... .......... .......... .......... .......... 60% 8.20M 9s
161900K .......... .......... .......... .......... .......... 60% 9.64M 9s
161950K .......... .......... .......... .......... .......... 61% 8.34M 9s
162000K .......... .......... .......... .......... .......... 61% 8.94M 9s
162050K .......... .......... .......... .......... .......... 61% 11.7M 9s
162100K .......... .......... .......... .......... .......... 61% 9.08M 9s
162150K .......... .......... .......... .......... .......... 61% 11.9M 9s
162200K .......... .......... .......... .......... .......... 61% 8.75M 9s
162250K .......... .......... .......... .......... .......... 61% 10.9M 9s
162300K .......... .......... .......... .......... .......... 61% 8.81M 9s
162350K .......... .......... .......... .......... .......... 61% 9.42M 9s
162400K .......... .......... .......... .......... .......... 61% 11.2M 9s
162450K .......... .......... .......... .......... .......... 61% 8.45M 9s
162500K .......... .......... .......... .......... .......... 61% 15.9M 9s
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162600K .......... .......... .......... .......... .......... 61% 9.86M 9s
162650K .......... .......... .......... .......... .......... 61% 24.5M 9s
162700K .......... .......... .......... .......... .......... 61% 7.38M 9s
162750K .......... .......... .......... .......... .......... 61% 18.5M 9s
162800K .......... .......... .......... .......... .......... 61% 11.0M 9s
162850K .......... .......... .......... .......... .......... 61% 10.4M 9s
162900K .......... .......... .......... .......... .......... 61% 11.9M 9s
162950K .......... .......... .......... .......... .......... 61% 10.1M 9s
163000K .......... .......... .......... .......... .......... 61% 16.8M 9s
163050K .......... .......... .......... .......... .......... 61% 12.3M 9s
163100K .......... .......... .......... .......... .......... 61% 13.0M 9s
163150K .......... .......... .......... .......... .......... 61% 14.9M 9s
163200K .......... .......... .......... .......... .......... 61% 11.7M 9s
163250K .......... .......... .......... .......... .......... 61% 13.9M 9s
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163350K .......... .......... .......... .......... .......... 61% 11.0M 9s
163400K .......... .......... .......... .......... .......... 61% 17.2M 9s
163450K .......... .......... .......... .......... .......... 61% 13.8M 9s
163500K .......... .......... .......... .......... .......... 61% 13.7M 9s
163550K .......... .......... .......... .......... .......... 61% 10.8M 9s
163600K .......... .......... .......... .......... .......... 61% 11.0M 9s
163650K .......... .......... .......... .......... .......... 61% 18.6M 9s
163700K .......... .......... .......... .......... .......... 61% 12.3M 9s
163750K .......... .......... .......... .......... .......... 61% 12.8M 9s
163800K .......... .......... .......... .......... .......... 61% 16.5M 9s
163850K .......... .......... .......... .......... .......... 61% 17.7M 9s
163900K .......... .......... .......... .......... .......... 61% 11.6M 9s
163950K .......... .......... .......... .......... .......... 61% 11.9M 9s
164000K .......... .......... .......... .......... .......... 61% 16.3M 9s
164050K .......... .......... .......... .......... .......... 61% 34.4M 9s
164100K .......... .......... .......... .......... .......... 61% 10.9M 9s
164150K .......... .......... .......... .......... .......... 61% 14.0M 9s
164200K .......... .......... .......... .......... .......... 61% 10.9M 9s
164250K .......... .......... .......... .......... .......... 61% 45.5M 9s
164300K .......... .......... .......... .......... .......... 61% 12.8M 9s
164350K .......... .......... .......... .......... .......... 61% 12.5M 9s
164400K .......... .......... .......... .......... .......... 61% 18.8M 9s
164450K .......... .......... .......... .......... .......... 61% 13.0M 9s
164500K .......... .......... .......... .......... .......... 61% 13.5M 9s
164550K .......... .......... .......... .......... .......... 61% 26.3M 9s
164600K .......... .......... .......... .......... .......... 62% 10.7M 9s
164650K .......... .......... .......... .......... .......... 62% 14.3M 9s
164700K .......... .......... .......... .......... .......... 62% 12.5M 9s
164750K .......... .......... .......... .......... .......... 62% 13.0M 9s
164800K .......... .......... .......... .......... .......... 62% 18.4M 9s
164850K .......... .......... .......... .......... .......... 62% 15.3M 9s
164900K .......... .......... .......... .......... .......... 62% 13.5M 9s
164950K .......... .......... .......... .......... .......... 62% 15.9M 9s
165000K .......... .......... .......... .......... .......... 62% 16.9M 9s
165050K .......... .......... .......... .......... .......... 62% 15.5M 9s
165100K .......... .......... .......... .......... .......... 62% 17.5M 9s
165150K .......... .......... .......... .......... .......... 62% 15.6M 9s
165200K .......... .......... .......... .......... .......... 62% 18.7M 9s
165250K .......... .......... .......... .......... .......... 62% 48.7M 9s
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165350K .......... .......... .......... .......... .......... 62% 16.8M 9s
165400K .......... .......... .......... .......... .......... 62% 27.9M 9s
165450K .......... .......... .......... .......... .......... 62% 17.9M 9s
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165550K .......... .......... .......... .......... .......... 62% 30.4M 9s
165600K .......... .......... .......... .......... .......... 62% 16.7M 9s
165650K .......... .......... .......... .......... .......... 62% 13.8M 9s
165700K .......... .......... .......... .......... .......... 62% 41.3M 9s
165750K .......... .......... .......... .......... .......... 62% 14.9M 9s
165800K .......... .......... .......... .......... .......... 62% 16.9M 9s
165850K .......... .......... .......... .......... .......... 62% 26.8M 9s
165900K .......... .......... .......... .......... .......... 62% 18.0M 9s
165950K .......... .......... .......... .......... .......... 62% 17.8M 9s
166000K .......... .......... .......... .......... .......... 62% 38.7M 9s
166050K .......... .......... .......... .......... .......... 62% 12.9M 9s
166100K .......... .......... .......... .......... .......... 62% 57.2M 9s
166150K .......... .......... .......... .......... .......... 62% 10.8M 9s
166200K .......... .......... .......... .......... .......... 62% 13.8M 9s
166250K .......... .......... .......... .......... .......... 62% 43.6M 9s
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166400K .......... .......... .......... .......... .......... 62% 15.6M 9s
166450K .......... .......... .......... .......... .......... 62% 40.1M 9s
166500K .......... .......... .......... .......... .......... 62% 14.5M 9s
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166600K .......... .......... .......... .......... .......... 62% 12.7M 9s
166650K .......... .......... .......... .......... .......... 62% 42.1M 9s
166700K .......... .......... .......... .......... .......... 62% 12.1M 9s
166750K .......... .......... .......... .......... .......... 62% 38.1M 9s
166800K .......... .......... .......... .......... .......... 62% 26.9M 9s
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166900K .......... .......... .......... .......... .......... 62% 35.6M 9s
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167000K .......... .......... .......... .......... .......... 62% 22.9M 9s
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167100K .......... .......... .......... .......... .......... 62% 14.7M 9s
167150K .......... .......... .......... .......... .......... 62% 32.1M 9s
167200K .......... .......... .......... .......... .......... 62% 13.8M 9s
167250K .......... .......... .......... .......... .......... 63% 43.0M 9s
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167400K .......... .......... .......... .......... .......... 63% 17.5M 9s
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167500K .......... .......... .......... .......... .......... 63% 34.1M 9s
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167600K .......... .......... .......... .......... .......... 63% 15.3M 9s
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167850K .......... .......... .......... .......... .......... 63% 14.5M 9s
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168000K .......... .......... .......... .......... .......... 63% 41.0M 9s
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168100K .......... .......... .......... .......... .......... 63% 27.6M 9s
168150K .......... .......... .......... .......... .......... 63% 8.46M 9s
168200K .......... .......... .......... .......... .......... 63% 65.2M 9s
168250K .......... .......... .......... .......... .......... 63% 36.3M 9s
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169000K .......... .......... .......... .......... .......... 63% 22.1M 8s
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169100K .......... .......... .......... .......... .......... 63% 13.1M 8s
169150K .......... .......... .......... .......... .......... 63% 62.8M 8s
169200K .......... .......... .......... .......... .......... 63% 20.1M 8s
169250K .......... .......... .......... .......... .......... 63% 18.8M 8s
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169500K .......... .......... .......... .......... .......... 63% 79.0M 8s
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170000K .......... .......... .......... .......... .......... 64% 19.1M 8s
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170100K .......... .......... .......... .......... .......... 64% 13.1M 8s
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170200K .......... .......... .......... .......... .......... 64% 16.9M 8s
170250K .......... .......... .......... .......... .......... 64% 13.9M 8s
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170350K .......... .......... .......... .......... .......... 64% 14.8M 8s
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171000K .......... .......... .......... .......... .......... 64% 16.3M 8s
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171100K .......... .......... .......... .......... .......... 64% 10.5M 8s
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171200K .......... .......... .......... .......... .......... 64% 7.94M 8s
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171500K .......... .......... .......... .......... .......... 64% 13.9M 8s
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171600K .......... .......... .......... .......... .......... 64% 12.7M 8s
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171700K .......... .......... .......... .......... .......... 64% 9.98M 8s
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171800K .......... .......... .......... .......... .......... 64% 12.1M 8s
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172150K .......... .......... .......... .......... .......... 64% 44.5M 8s
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172250K .......... .......... .......... .......... .......... 64% 13.2M 8s
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172500K .......... .......... .......... .......... .......... 64% 13.5M 8s
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172600K .......... .......... .......... .......... .......... 65% 16.4M 8s
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172700K .......... .......... .......... .......... .......... 65% 11.5M 8s
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172800K .......... .......... .......... .......... .......... 65% 13.2M 8s
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172900K .......... .......... .......... .......... .......... 65% 20.0M 8s
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173000K .......... .......... .......... .......... .......... 65% 12.7M 8s
173050K .......... .......... .......... .......... .......... 65% 18.7M 8s
173100K .......... .......... .......... .......... .......... 65% 10.2M 8s
173150K .......... .......... .......... .......... .......... 65% 21.9M 8s
173200K .......... .......... .......... .......... .......... 65% 13.2M 8s
173250K .......... .......... .......... .......... .......... 65% 10.0M 8s
173300K .......... .......... .......... .......... .......... 65% 35.2M 8s
173350K .......... .......... .......... .......... .......... 65% 9.82M 8s
173400K .......... .......... .......... .......... .......... 65% 37.2M 8s
173450K .......... .......... .......... .......... .......... 65% 9.84M 8s
173500K .......... .......... .......... .......... .......... 65% 18.3M 8s
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173600K .......... .......... .......... .......... .......... 65% 11.5M 8s
173650K .......... .......... .......... .......... .......... 65% 14.0M 8s
173700K .......... .......... .......... .......... .......... 65% 15.2M 8s
173750K .......... .......... .......... .......... .......... 65% 18.9M 8s
173800K .......... .......... .......... .......... .......... 65% 14.0M 8s
173850K .......... .......... .......... .......... .......... 65% 21.7M 8s
173900K .......... .......... .......... .......... .......... 65% 18.0M 8s
173950K .......... .......... .......... .......... .......... 65% 19.0M 8s
174000K .......... .......... .......... .......... .......... 65% 13.8M 8s
174050K .......... .......... .......... .......... .......... 65% 14.7M 8s
174100K .......... .......... .......... .......... .......... 65% 18.6M 8s
174150K .......... .......... .......... .......... .......... 65% 15.2M 8s
174200K .......... .......... .......... .......... .......... 65% 15.0M 8s
174250K .......... .......... .......... .......... .......... 65% 23.7M 8s
174300K .......... .......... .......... .......... .......... 65% 14.6M 8s
174350K .......... .......... .......... .......... .......... 65% 21.2M 8s
174400K .......... .......... .......... .......... .......... 65% 14.9M 8s
174450K .......... .......... .......... .......... .......... 65% 14.8M 8s
174500K .......... .......... .......... .......... .......... 65% 27.2M 8s
174550K .......... .......... .......... .......... .......... 65% 19.0M 8s
174600K .......... .......... .......... .......... .......... 65% 19.2M 8s
174650K .......... .......... .......... .......... .......... 65% 14.1M 8s
174700K .......... .......... .......... .......... .......... 65% 42.9M 8s
174750K .......... .......... .......... .......... .......... 65% 15.5M 8s
174800K .......... .......... .......... .......... .......... 65% 17.1M 8s
174850K .......... .......... .......... .......... .......... 65% 22.2M 8s
174900K .......... .......... .......... .......... .......... 65% 17.8M 8s
174950K .......... .......... .......... .......... .......... 65% 40.3M 8s
175000K .......... .......... .......... .......... .......... 65% 13.9M 8s
175050K .......... .......... .......... .......... .......... 65% 45.4M 8s
175100K .......... .......... .......... .......... .......... 65% 15.5M 8s
175150K .......... .......... .......... .......... .......... 65% 41.0M 8s
175200K .......... .......... .......... .......... .......... 66% 11.7M 8s
175250K .......... .......... .......... .......... .......... 66% 57.2M 8s
175300K .......... .......... .......... .......... .......... 66% 15.5M 8s
175350K .......... .......... .......... .......... .......... 66% 15.0M 8s
175400K .......... .......... .......... .......... .......... 66% 38.7M 8s
175450K .......... .......... .......... .......... .......... 66% 17.5M 8s
175500K .......... .......... .......... .......... .......... 66% 59.0M 8s
175550K .......... .......... .......... .......... .......... 66% 12.7M 8s
175600K .......... .......... .......... .......... .......... 66% 31.8M 8s
175650K .......... .......... .......... .......... .......... 66% 21.8M 8s
175700K .......... .......... .......... .......... .......... 66% 22.1M 8s
175750K .......... .......... .......... .......... .......... 66% 24.3M 8s
175800K .......... .......... .......... .......... .......... 66% 21.9M 8s
175850K .......... .......... .......... .......... .......... 66% 20.9M 8s
175900K .......... .......... .......... .......... .......... 66% 19.7M 8s
175950K .......... .......... .......... .......... .......... 66% 16.0M 8s
176000K .......... .......... .......... .......... .......... 66% 30.8M 8s
176050K .......... .......... .......... .......... .......... 66% 17.1M 8s
176100K .......... .......... .......... .......... .......... 66% 28.6M 8s
176150K .......... .......... .......... .......... .......... 66% 14.5M 8s
176200K .......... .......... .......... .......... .......... 66% 21.1M 8s
176250K .......... .......... .......... .......... .......... 66% 26.7M 8s
176300K .......... .......... .......... .......... .......... 66% 18.4M 8s
176350K .......... .......... .......... .......... .......... 66% 22.4M 8s
176400K .......... .......... .......... .......... .......... 66% 21.0M 8s
176450K .......... .......... .......... .......... .......... 66% 19.4M 8s
176500K .......... .......... .......... .......... .......... 66% 17.9M 8s
176550K .......... .......... .......... .......... .......... 66% 18.1M 8s
176600K .......... .......... .......... .......... .......... 66% 21.9M 8s
176650K .......... .......... .......... .......... .......... 66% 18.5M 8s
176700K .......... .......... .......... .......... .......... 66% 21.9M 8s
176750K .......... .......... .......... .......... .......... 66% 18.4M 8s
176800K .......... .......... .......... .......... .......... 66% 12.1M 8s
176850K .......... .......... .......... .......... .......... 66% 65.3M 8s
176900K .......... .......... .......... .......... .......... 66% 20.4M 8s
176950K .......... .......... .......... .......... .......... 66% 5.98M 8s
177000K .......... .......... .......... .......... .......... 66% 152M 8s
177050K .......... .......... .......... .......... .......... 66% 55.6M 8s
177100K .......... .......... .......... .......... .......... 66% 15.2M 8s
177150K .......... .......... .......... .......... .......... 66% 16.3M 8s
177200K .......... .......... .......... .......... .......... 66% 11.0M 8s
177250K .......... .......... .......... .......... .......... 66% 16.5M 8s
177300K .......... .......... .......... .......... .......... 66% 19.9M 8s
177350K .......... .......... .......... .......... .......... 66% 10.4M 8s
177400K .......... .......... .......... .......... .......... 66% 20.0M 8s
177450K .......... .......... .......... .......... .......... 66% 12.4M 8s
177500K .......... .......... .......... .......... .......... 66% 17.4M 8s
177550K .......... .......... .......... .......... .......... 66% 14.4M 8s
177600K .......... .......... .......... .......... .......... 66% 9.80M 8s
177650K .......... .......... .......... .......... .......... 66% 12.3M 8s
177700K .......... .......... .......... .......... .......... 66% 18.9M 8s
177750K .......... .......... .......... .......... .......... 66% 17.8M 8s
177800K .......... .......... .......... .......... .......... 66% 22.0M 8s
177850K .......... .......... .......... .......... .......... 67% 14.4M 8s
177900K .......... .......... .......... .......... .......... 67% 14.9M 8s
177950K .......... .......... .......... .......... .......... 67% 16.3M 8s
178000K .......... .......... .......... .......... .......... 67% 13.4M 8s
178050K .......... .......... .......... .......... .......... 67% 11.9M 8s
178100K .......... .......... .......... .......... .......... 67% 19.5M 8s
178150K .......... .......... .......... .......... .......... 67% 13.0M 8s
178200K .......... .......... .......... .......... .......... 67% 12.5M 8s
178250K .......... .......... .......... .......... .......... 67% 12.6M 7s
178300K .......... .......... .......... .......... .......... 67% 14.6M 7s
178350K .......... .......... .......... .......... .......... 67% 15.9M 7s
178400K .......... .......... .......... .......... .......... 67% 21.5M 7s
178450K .......... .......... .......... .......... .......... 67% 14.0M 7s
178500K .......... .......... .......... .......... .......... 67% 12.7M 7s
178550K .......... .......... .......... .......... .......... 67% 9.19M 7s
178600K .......... .......... .......... .......... .......... 67% 26.5M 7s
178650K .......... .......... .......... .......... .......... 67% 12.3M 7s
178700K .......... .......... .......... .......... .......... 67% 13.2M 7s
178750K .......... .......... .......... .......... .......... 67% 13.0M 7s
178800K .......... .......... .......... .......... .......... 67% 29.2M 7s
178850K .......... .......... .......... .......... .......... 67% 11.2M 7s
178900K .......... .......... .......... .......... .......... 67% 15.2M 7s
178950K .......... .......... .......... .......... .......... 67% 13.6M 7s
179000K .......... .......... .......... .......... .......... 67% 12.2M 7s
179050K .......... .......... .......... .......... .......... 67% 13.2M 7s
179100K .......... .......... .......... .......... .......... 67% 14.6M 7s
179150K .......... .......... .......... .......... .......... 67% 15.5M 7s
179200K .......... .......... .......... .......... .......... 67% 9.69M 7s
179250K .......... .......... .......... .......... .......... 67% 14.6M 7s
179300K .......... .......... .......... .......... .......... 67% 17.7M 7s
179350K .......... .......... .......... .......... .......... 67% 16.5M 7s
179400K .......... .......... .......... .......... .......... 67% 4.99M 7s
179450K .......... .......... .......... .......... .......... 67% 52.4M 7s
179500K .......... .......... .......... .......... .......... 67% 72.3M 7s
179550K .......... .......... .......... .......... .......... 67% 16.9M 7s
179600K .......... .......... .......... .......... .......... 67% 12.3M 7s
179650K .......... .......... .......... .......... .......... 67% 11.9M 7s
179700K .......... .......... .......... .......... .......... 67% 13.2M 7s
179750K .......... .......... .......... .......... .......... 67% 31.0M 7s
179800K .......... .......... .......... .......... .......... 67% 12.5M 7s
179850K .......... .......... .......... .......... .......... 67% 11.7M 7s
179900K .......... .......... .......... .......... .......... 67% 18.2M 7s
179950K .......... .......... .......... .......... .......... 67% 10.9M 7s
180000K .......... .......... .......... .......... .......... 67% 63.2M 7s
180050K .......... .......... .......... .......... .......... 67% 11.4M 7s
180100K .......... .......... .......... .......... .......... 67% 11.9M 7s
180150K .......... .......... .......... .......... .......... 67% 25.5M 7s
180200K .......... .......... .......... .......... .......... 67% 20.1M 7s
180250K .......... .......... .......... .......... .......... 67% 13.1M 7s
180300K .......... .......... .......... .......... .......... 67% 13.0M 7s
180350K .......... .......... .......... .......... .......... 67% 11.1M 7s
180400K .......... .......... .......... .......... .......... 67% 21.1M 7s
180450K .......... .......... .......... .......... .......... 67% 11.6M 7s
180500K .......... .......... .......... .......... .......... 68% 21.6M 7s
180550K .......... .......... .......... .......... .......... 68% 14.4M 7s
180600K .......... .......... .......... .......... .......... 68% 12.4M 7s
180650K .......... .......... .......... .......... .......... 68% 20.3M 7s
180700K .......... .......... .......... .......... .......... 68% 15.9M 7s
180750K .......... .......... .......... .......... .......... 68% 10.7M 7s
180800K .......... .......... .......... .......... .......... 68% 13.9M 7s
180850K .......... .......... .......... .......... .......... 68% 17.8M 7s
180900K .......... .......... .......... .......... .......... 68% 12.8M 7s
180950K .......... .......... .......... .......... .......... 68% 14.3M 7s
181000K .......... .......... .......... .......... .......... 68% 13.7M 7s
181050K .......... .......... .......... .......... .......... 68% 10.6M 7s
181100K .......... .......... .......... .......... .......... 68% 12.8M 7s
181150K .......... .......... .......... .......... .......... 68% 12.2M 7s
181200K .......... .......... .......... .......... .......... 68% 19.3M 7s
181250K .......... .......... .......... .......... .......... 68% 13.9M 7s
181300K .......... .......... .......... .......... .......... 68% 13.2M 7s
181350K .......... .......... .......... .......... .......... 68% 22.7M 7s
181400K .......... .......... .......... .......... .......... 68% 15.1M 7s
181450K .......... .......... .......... .......... .......... 68% 22.8M 7s
181500K .......... .......... .......... .......... .......... 68% 12.0M 7s
181550K .......... .......... .......... .......... .......... 68% 14.2M 7s
181600K .......... .......... .......... .......... .......... 68% 15.2M 7s
181650K .......... .......... .......... .......... .......... 68% 17.8M 7s
181700K .......... .......... .......... .......... .......... 68% 5.55M 7s
181750K .......... .......... .......... .......... .......... 68% 43.8M 7s
181800K .......... .......... .......... .......... .......... 68% 32.8M 7s
181850K .......... .......... .......... .......... .......... 68% 10.5M 7s
181900K .......... .......... .......... .......... .......... 68% 35.6M 7s
181950K .......... .......... .......... .......... .......... 68% 11.0M 7s
182000K .......... .......... .......... .......... .......... 68% 11.9M 7s
182050K .......... .......... .......... .......... .......... 68% 14.0M 7s
182100K .......... .......... .......... .......... .......... 68% 10.8M 7s
182150K .......... .......... .......... .......... .......... 68% 10.9M 7s
182200K .......... .......... .......... .......... .......... 68% 11.2M 7s
182250K .......... .......... .......... .......... .......... 68% 13.9M 7s
182300K .......... .......... .......... .......... .......... 68% 16.1M 7s
182350K .......... .......... .......... .......... .......... 68% 26.5M 7s
182400K .......... .......... .......... .......... .......... 68% 12.0M 7s
182450K .......... .......... .......... .......... .......... 68% 10.3M 7s
182500K .......... .......... .......... .......... .......... 68% 14.5M 7s
182550K .......... .......... .......... .......... .......... 68% 14.2M 7s
182600K .......... .......... .......... .......... .......... 68% 25.5M 7s
182650K .......... .......... .......... .......... .......... 68% 15.5M 7s
182700K .......... .......... .......... .......... .......... 68% 12.0M 7s
182750K .......... .......... .......... .......... .......... 68% 15.5M 7s
182800K .......... .......... .......... .......... .......... 68% 17.5M 7s
182850K .......... .......... .......... .......... .......... 68% 17.8M 7s
182900K .......... .......... .......... .......... .......... 68% 12.4M 7s
182950K .......... .......... .......... .......... .......... 68% 14.2M 7s
183000K .......... .......... .......... .......... .......... 68% 14.3M 7s
183050K .......... .......... .......... .......... .......... 68% 21.4M 7s
183100K .......... .......... .......... .......... .......... 68% 10.7M 7s
183150K .......... .......... .......... .......... .......... 68% 14.5M 7s
183200K .......... .......... .......... .......... .......... 69% 13.7M 7s
183250K .......... .......... .......... .......... .......... 69% 20.4M 7s
183300K .......... .......... .......... .......... .......... 69% 13.0M 7s
183350K .......... .......... .......... .......... .......... 69% 16.8M 7s
183400K .......... .......... .......... .......... .......... 69% 9.90M 7s
183450K .......... .......... .......... .......... .......... 69% 26.7M 7s
183500K .......... .......... .......... .......... .......... 69% 12.7M 7s
183550K .......... .......... .......... .......... .......... 69% 20.2M 7s
183600K .......... .......... .......... .......... .......... 69% 11.6M 7s
183650K .......... .......... .......... .......... .......... 69% 16.3M 7s
183700K .......... .......... .......... .......... .......... 69% 12.8M 7s
183750K .......... .......... .......... .......... .......... 69% 17.3M 7s
183800K .......... .......... .......... .......... .......... 69% 15.0M 7s
183850K .......... .......... .......... .......... .......... 69% 11.5M 7s
183900K .......... .......... .......... .......... .......... 69% 13.9M 7s
183950K .......... .......... .......... .......... .......... 69% 11.6M 7s
184000K .......... .......... .......... .......... .......... 69% 22.2M 7s
184050K .......... .......... .......... .......... .......... 69% 16.3M 7s
184100K .......... .......... .......... .......... .......... 69% 11.4M 7s
184150K .......... .......... .......... .......... .......... 69% 21.3M 7s
184200K .......... .......... .......... .......... .......... 69% 5.31M 7s
184250K .......... .......... .......... .......... .......... 69% 107M 7s
184300K .......... .......... .......... .......... .......... 69% 73.6M 7s
184350K .......... .......... .......... .......... .......... 69% 12.0M 7s
184400K .......... .......... .......... .......... .......... 69% 11.8M 7s
184450K .......... .......... .......... .......... .......... 69% 12.4M 7s
184500K .......... .......... .......... .......... .......... 69% 12.6M 7s
184550K .......... .......... .......... .......... .......... 69% 12.0M 7s
184600K .......... .......... .......... .......... .......... 69% 9.64M 7s
184650K .......... .......... .......... .......... .......... 69% 13.0M 7s
184700K .......... .......... .......... .......... .......... 69% 11.7M 7s
184750K .......... .......... .......... .......... .......... 69% 16.0M 7s
184800K .......... .......... .......... .......... .......... 69% 10.7M 7s
184850K .......... .......... .......... .......... .......... 69% 12.2M 7s
184900K .......... .......... .......... .......... .......... 69% 18.8M 7s
184950K .......... .......... .......... .......... .......... 69% 5.08M 7s
185000K .......... .......... .......... .......... .......... 69% 99.1M 7s
185050K .......... .......... .......... .......... .......... 69% 12.9M 7s
185100K .......... .......... .......... .......... .......... 69% 7.68M 7s
185150K .......... .......... .......... .......... .......... 69% 11.9M 7s
185200K .......... .......... .......... .......... .......... 69% 8.27M 7s
185250K .......... .......... .......... .......... .......... 69% 9.27M 7s
185300K .......... .......... .......... .......... .......... 69% 10.9M 7s
185350K .......... .......... .......... .......... .......... 69% 7.42M 7s
185400K .......... .......... .......... .......... .......... 69% 12.1M 7s
185450K .......... .......... .......... .......... .......... 69% 12.2M 7s
185500K .......... .......... .......... .......... .......... 69% 7.84M 7s
185550K .......... .......... .......... .......... .......... 69% 13.1M 7s
185600K .......... .......... .......... .......... .......... 69% 8.38M 7s
185650K .......... .......... .......... .......... .......... 69% 11.1M 7s
185700K .......... .......... .......... .......... .......... 69% 11.3M 7s
185750K .......... .......... .......... .......... .......... 69% 12.0M 7s
185800K .......... .......... .......... .......... .......... 69% 12.0M 7s
185850K .......... .......... .......... .......... .......... 70% 10.6M 7s
185900K .......... .......... .......... .......... .......... 70% 9.69M 7s
185950K .......... .......... .......... .......... .......... 70% 9.07M 7s
186000K .......... .......... .......... .......... .......... 70% 10.3M 7s
186050K .......... .......... .......... .......... .......... 70% 10.8M 7s
186100K .......... .......... .......... .......... .......... 70% 6.75M 7s
186150K .......... .......... .......... .......... .......... 70% 22.7M 7s
186200K .......... .......... .......... .......... .......... 70% 6.07M 7s
186250K .......... .......... .......... .......... .......... 70% 11.4M 7s
186300K .......... .......... .......... .......... .......... 70% 11.0M 7s
186350K .......... .......... .......... .......... .......... 70% 6.07M 7s
186400K .......... .......... .......... .......... .......... 70% 10.4M 7s
186450K .......... .......... .......... .......... .......... 70% 9.62M 7s
186500K .......... .......... .......... .......... .......... 70% 9.74M 7s
186550K .......... .......... .......... .......... .......... 70% 8.62M 7s
186600K .......... .......... .......... .......... .......... 70% 8.49M 7s
186650K .......... .......... .......... .......... .......... 70% 11.1M 7s
186700K .......... .......... .......... .......... .......... 70% 9.15M 7s
186750K .......... .......... .......... .......... .......... 70% 7.77M 7s
186800K .......... .......... .......... .......... .......... 70% 7.95M 7s
186850K .......... .......... .......... .......... .......... 70% 10.5M 7s
186900K .......... .......... .......... .......... .......... 70% 10.3M 7s
186950K .......... .......... .......... .......... .......... 70% 9.36M 7s
187000K .......... .......... .......... .......... .......... 70% 10.5M 7s
187050K .......... .......... .......... .......... .......... 70% 8.55M 7s
187100K .......... .......... .......... .......... .......... 70% 7.55M 7s
187150K .......... .......... .......... .......... .......... 70% 10.6M 7s
187200K .......... .......... .......... .......... .......... 70% 8.94M 7s
187250K .......... .......... .......... .......... .......... 70% 11.2M 7s
187300K .......... .......... .......... .......... .......... 70% 15.0M 7s
187350K .......... .......... .......... .......... .......... 70% 7.58M 7s
187400K .......... .......... .......... .......... .......... 70% 19.5M 7s
187450K .......... .......... .......... .......... .......... 70% 10.3M 7s
187500K .......... .......... .......... .......... .......... 70% 11.2M 7s
187550K .......... .......... .......... .......... .......... 70% 16.5M 7s
187600K .......... .......... .......... .......... .......... 70% 13.3M 7s
187650K .......... .......... .......... .......... .......... 70% 10.7M 7s
187700K .......... .......... .......... .......... .......... 70% 9.78M 7s
187750K .......... .......... .......... .......... .......... 70% 9.89M 7s
187800K .......... .......... .......... .......... .......... 70% 11.3M 7s
187850K .......... .......... .......... .......... .......... 70% 10.7M 7s
187900K .......... .......... .......... .......... .......... 70% 11.4M 7s
187950K .......... .......... .......... .......... .......... 70% 10.4M 7s
188000K .......... .......... .......... .......... .......... 70% 12.5M 7s
188050K .......... .......... .......... .......... .......... 70% 13.1M 7s
188100K .......... .......... .......... .......... .......... 70% 11.6M 7s
188150K .......... .......... .......... .......... .......... 70% 14.5M 7s
188200K .......... .......... .......... .......... .......... 70% 11.3M 7s
188250K .......... .......... .......... .......... .......... 70% 17.6M 7s
188300K .......... .......... .......... .......... .......... 70% 13.5M 7s
188350K .......... .......... .......... .......... .......... 70% 15.1M 7s
188400K .......... .......... .......... .......... .......... 70% 24.9M 7s
188450K .......... .......... .......... .......... .......... 70% 14.6M 7s
188500K .......... .......... .......... .......... .......... 71% 16.2M 7s
188550K .......... .......... .......... .......... .......... 71% 13.5M 7s
188600K .......... .......... .......... .......... .......... 71% 12.7M 7s
188650K .......... .......... .......... .......... .......... 71% 64.9M 7s
188700K .......... .......... .......... .......... .......... 71% 10.0M 7s
188750K .......... .......... .......... .......... .......... 71% 16.1M 7s
188800K .......... .......... .......... .......... .......... 71% 16.3M 7s
188850K .......... .......... .......... .......... .......... 71% 15.8M 7s
188900K .......... .......... .......... .......... .......... 71% 15.6M 7s
188950K .......... .......... .......... .......... .......... 71% 9.10M 7s
189000K .......... .......... .......... .......... .......... 71% 40.5M 7s
189050K .......... .......... .......... .......... .......... 71% 14.2M 7s
189100K .......... .......... .......... .......... .......... 71% 12.6M 7s
189150K .......... .......... .......... .......... .......... 71% 15.9M 7s
189200K .......... .......... .......... .......... .......... 71% 13.0M 7s
189250K .......... .......... .......... .......... .......... 71% 19.8M 7s
189300K .......... .......... .......... .......... .......... 71% 13.9M 7s
189350K .......... .......... .......... .......... .......... 71% 15.5M 7s
189400K .......... .......... .......... .......... .......... 71% 17.9M 6s
189450K .......... .......... .......... .......... .......... 71% 13.8M 6s
189500K .......... .......... .......... .......... .......... 71% 16.9M 6s
189550K .......... .......... .......... .......... .......... 71% 14.3M 6s
189600K .......... .......... .......... .......... .......... 71% 10.3M 6s
189650K .......... .......... .......... .......... .......... 71% 14.5M 6s
189700K .......... .......... .......... .......... .......... 71% 19.9M 6s
189750K .......... .......... .......... .......... .......... 71% 14.7M 6s
189800K .......... .......... .......... .......... .......... 71% 11.3M 6s
189850K .......... .......... .......... .......... .......... 71% 12.4M 6s
189900K .......... .......... .......... .......... .......... 71% 22.9M 6s
189950K .......... .......... .......... .......... .......... 71% 12.4M 6s
190000K .......... .......... .......... .......... .......... 71% 13.2M 6s
190050K .......... .......... .......... .......... .......... 71% 20.2M 6s
190100K .......... .......... .......... .......... .......... 71% 14.1M 6s
190150K .......... .......... .......... .......... .......... 71% 18.0M 6s
190200K .......... .......... .......... .......... .......... 71% 12.4M 6s
190250K .......... .......... .......... .......... .......... 71% 15.2M 6s
190300K .......... .......... .......... .......... .......... 71% 5.68M 6s
190350K .......... .......... .......... .......... .......... 71% 33.4M 6s
190400K .......... .......... .......... .......... .......... 71% 69.5M 6s
190450K .......... .......... .......... .......... .......... 71% 12.1M 6s
190500K .......... .......... .......... .......... .......... 71% 10.9M 6s
190550K .......... .......... .......... .......... .......... 71% 11.5M 6s
190600K .......... .......... .......... .......... .......... 71% 4.77M 6s
190650K .......... .......... .......... .......... .......... 71% 148M 6s
190700K .......... .......... .......... .......... .......... 71% 9.44M 6s
190750K .......... .......... .......... .......... .......... 71% 13.1M 6s
190800K .......... .......... .......... .......... .......... 71% 11.0M 6s
190850K .......... .......... .......... .......... .......... 71% 12.4M 6s
190900K .......... .......... .......... .......... .......... 71% 12.5M 6s
190950K .......... .......... .......... .......... .......... 71% 7.24M 6s
191000K .......... .......... .......... .......... .......... 71% 12.2M 6s
191050K .......... .......... .......... .......... .......... 71% 12.3M 6s
191100K .......... .......... .......... .......... .......... 71% 9.99M 6s
191150K .......... .......... .......... .......... .......... 72% 13.0M 6s
191200K .......... .......... .......... .......... .......... 72% 12.9M 6s
191250K .......... .......... .......... .......... .......... 72% 10.3M 6s
191300K .......... .......... .......... .......... .......... 72% 12.3M 6s
191350K .......... .......... .......... .......... .......... 72% 11.4M 6s
191400K .......... .......... .......... .......... .......... 72% 10.4M 6s
191450K .......... .......... .......... .......... .......... 72% 7.14M 6s
191500K .......... .......... .......... .......... .......... 72% 6.41M 6s
191550K .......... .......... .......... .......... .......... 72% 23.8M 6s
191600K .......... .......... .......... .......... .......... 72% 4.47M 6s
191650K .......... .......... .......... .......... .......... 72% 5.25M 6s
191700K .......... .......... .......... .......... .......... 72% 6.42M 6s
191750K .......... .......... .......... .......... .......... 72% 6.13M 6s
191800K .......... .......... .......... .......... .......... 72% 5.99M 6s
191850K .......... .......... .......... .......... .......... 72% 5.45M 6s
191900K .......... .......... .......... .......... .......... 72% 7.67M 6s
191950K .......... .......... .......... .......... .......... 72% 6.15M 6s
192000K .......... .......... .......... .......... .......... 72% 8.28M 6s
192050K .......... .......... .......... .......... .......... 72% 5.30M 6s
192100K .......... .......... .......... .......... .......... 72% 7.68M 6s
192150K .......... .......... .......... .......... .......... 72% 7.95M 6s
192200K .......... .......... .......... .......... .......... 72% 7.21M 6s
192250K .......... .......... .......... .......... .......... 72% 9.70M 6s
192300K .......... .......... .......... .......... .......... 72% 8.46M 6s
192350K .......... .......... .......... .......... .......... 72% 8.13M 6s
192400K .......... .......... .......... .......... .......... 72% 7.32M 6s
192450K .......... .......... .......... .......... .......... 72% 8.24M 6s
192500K .......... .......... .......... .......... .......... 72% 5.71M 6s
192550K .......... .......... .......... .......... .......... 72% 8.57M 6s
192600K .......... .......... .......... .......... .......... 72% 4.93M 6s
192650K .......... .......... .......... .......... .......... 72% 7.66M 6s
192700K .......... .......... .......... .......... .......... 72% 5.32M 6s
192750K .......... .......... .......... .......... .......... 72% 7.20M 6s
192800K .......... .......... .......... .......... .......... 72% 7.52M 6s
192850K .......... .......... .......... .......... .......... 72% 4.28M 6s
192900K .......... .......... .......... .......... .......... 72% 11.6M 6s
192950K .......... .......... .......... .......... .......... 72% 4.25M 6s
193000K .......... .......... .......... .......... .......... 72% 6.10M 6s
193050K .......... .......... .......... .......... .......... 72% 6.43M 6s
193100K .......... .......... .......... .......... .......... 72% 6.26M 6s
193150K .......... .......... .......... .......... .......... 72% 6.41M 6s
193200K .......... .......... .......... .......... .......... 72% 5.70M 6s
193250K .......... .......... .......... .......... .......... 72% 12.4M 6s
193300K .......... .......... .......... .......... .......... 72% 5.94M 6s
193350K .......... .......... .......... .......... .......... 72% 5.61M 6s
193400K .......... .......... .......... .......... .......... 72% 12.3M 6s
193450K .......... .......... .......... .......... .......... 72% 6.23M 6s
193500K .......... .......... .......... .......... .......... 72% 8.17M 6s
193550K .......... .......... .......... .......... .......... 72% 10.7M 6s
193600K .......... .......... .......... .......... .......... 72% 6.09M 6s
193650K .......... .......... .......... .......... .......... 72% 10.4M 6s
193700K .......... .......... .......... .......... .......... 72% 6.99M 6s
193750K .......... .......... .......... .......... .......... 72% 12.8M 6s
193800K .......... .......... .......... .......... .......... 73% 10.9M 6s
193850K .......... .......... .......... .......... .......... 73% 11.1M 6s
193900K .......... .......... .......... .......... .......... 73% 12.1M 6s
193950K .......... .......... .......... .......... .......... 73% 6.68M 6s
194000K .......... .......... .......... .......... .......... 73% 9.76M 6s
194050K .......... .......... .......... .......... .......... 73% 11.7M 6s
194100K .......... .......... .......... .......... .......... 73% 11.8M 6s
194150K .......... .......... .......... .......... .......... 73% 5.34M 6s
194200K .......... .......... .......... .......... .......... 73% 16.8M 6s
194250K .......... .......... .......... .......... .......... 73% 14.6M 6s
194300K .......... .......... .......... .......... .......... 73% 7.37M 6s
194350K .......... .......... .......... .......... .......... 73% 9.78M 6s
194400K .......... .......... .......... .......... .......... 73% 7.25M 6s
194450K .......... .......... .......... .......... .......... 73% 5.40M 6s
194500K .......... .......... .......... .......... .......... 73% 14.9M 6s
194550K .......... .......... .......... .......... .......... 73% 7.23M 6s
194600K .......... .......... .......... .......... .......... 73% 10.6M 6s
194650K .......... .......... .......... .......... .......... 73% 10.8M 6s
194700K .......... .......... .......... .......... .......... 73% 6.32M 6s
194750K .......... .......... .......... .......... .......... 73% 10.4M 6s
194800K .......... .......... .......... .......... .......... 73% 10.7M 6s
194850K .......... .......... .......... .......... .......... 73% 6.69M 6s
194900K .......... .......... .......... .......... .......... 73% 11.8M 6s
194950K .......... .......... .......... .......... .......... 73% 10.1M 6s
195000K .......... .......... .......... .......... .......... 73% 11.6M 6s
195050K .......... .......... .......... .......... .......... 73% 9.81M 6s
195100K .......... .......... .......... .......... .......... 73% 7.60M 6s
195150K .......... .......... .......... .......... .......... 73% 9.42M 6s
195200K .......... .......... .......... .......... .......... 73% 5.32M 6s
195250K .......... .......... .......... .......... .......... 73% 52.4M 6s
195300K .......... .......... .......... .......... .......... 73% 8.46M 6s
195350K .......... .......... .......... .......... .......... 73% 9.32M 6s
195400K .......... .......... .......... .......... .......... 73% 6.62M 6s
195450K .......... .......... .......... .......... .......... 73% 12.2M 6s
195500K .......... .......... .......... .......... .......... 73% 6.23M 6s
195550K .......... .......... .......... .......... .......... 73% 10.5M 6s
195600K .......... .......... .......... .......... .......... 73% 5.96M 6s
195650K .......... .......... .......... .......... .......... 73% 10.4M 6s
195700K .......... .......... .......... .......... .......... 73% 6.79M 6s
195750K .......... .......... .......... .......... .......... 73% 7.23M 6s
195800K .......... .......... .......... .......... .......... 73% 11.6M 6s
195850K .......... .......... .......... .......... .......... 73% 8.13M 6s
195900K .......... .......... .......... .......... .......... 73% 7.49M 6s
195950K .......... .......... .......... .......... .......... 73% 9.65M 6s
196000K .......... .......... .......... .......... .......... 73% 11.6M 6s
196050K .......... .......... .......... .......... .......... 73% 10.2M 6s
196100K .......... .......... .......... .......... .......... 73% 7.67M 6s
196150K .......... .......... .......... .......... .......... 73% 11.6M 6s
196200K .......... .......... .......... .......... .......... 73% 8.64M 6s
196250K .......... .......... .......... .......... .......... 73% 12.7M 6s
196300K .......... .......... .......... .......... .......... 73% 10.9M 6s
196350K .......... .......... .......... .......... .......... 73% 12.0M 6s
196400K .......... .......... .......... .......... .......... 73% 11.4M 6s
196450K .......... .......... .......... .......... .......... 74% 8.00M 6s
196500K .......... .......... .......... .......... .......... 74% 13.7M 6s
196550K .......... .......... .......... .......... .......... 74% 8.43M 6s
196600K .......... .......... .......... .......... .......... 74% 11.8M 6s
196650K .......... .......... .......... .......... .......... 74% 10.0M 6s
196700K .......... .......... .......... .......... .......... 74% 5.22M 6s
196750K .......... .......... .......... .......... .......... 74% 109M 6s
196800K .......... .......... .......... .......... .......... 74% 13.1M 6s
196850K .......... .......... .......... .......... .......... 74% 6.99M 6s
196900K .......... .......... .......... .......... .......... 74% 12.3M 6s
196950K .......... .......... .......... .......... .......... 74% 13.4M 6s
197000K .......... .......... .......... .......... .......... 74% 9.49M 6s
197050K .......... .......... .......... .......... .......... 74% 8.27M 6s
197100K .......... .......... .......... .......... .......... 74% 10.9M 6s
197150K .......... .......... .......... .......... .......... 74% 11.6M 6s
197200K .......... .......... .......... .......... .......... 74% 6.76M 6s
197250K .......... .......... .......... .......... .......... 74% 9.47M 6s
197300K .......... .......... .......... .......... .......... 74% 11.9M 6s
197350K .......... .......... .......... .......... .......... 74% 7.78M 6s
197400K .......... .......... .......... .......... .......... 74% 12.3M 6s
197450K .......... .......... .......... .......... .......... 74% 5.42M 6s
197500K .......... .......... .......... .......... .......... 74% 15.5M 6s
197550K .......... .......... .......... .......... .......... 74% 5.91M 6s
197600K .......... .......... .......... .......... .......... 74% 7.87M 6s
197650K .......... .......... .......... .......... .......... 74% 10.5M 6s
197700K .......... .......... .......... .......... .......... 74% 6.55M 6s
197750K .......... .......... .......... .......... .......... 74% 8.73M 6s
197800K .......... .......... .......... .......... .......... 74% 7.21M 6s
197850K .......... .......... .......... .......... .......... 74% 8.01M 6s
197900K .......... .......... .......... .......... .......... 74% 11.1M 6s
197950K .......... .......... .......... .......... .......... 74% 5.86M 6s
198000K .......... .......... .......... .......... .......... 74% 9.62M 6s
198050K .......... .......... .......... .......... .......... 74% 8.87M 6s
198100K .......... .......... .......... .......... .......... 74% 8.52M 6s
198150K .......... .......... .......... .......... .......... 74% 11.4M 6s
198200K .......... .......... .......... .......... .......... 74% 7.97M 6s
198250K .......... .......... .......... .......... .......... 74% 12.2M 6s
198300K .......... .......... .......... .......... .......... 74% 8.17M 6s
198350K .......... .......... .......... .......... .......... 74% 10.9M 6s
198400K .......... .......... .......... .......... .......... 74% 11.4M 6s
198450K .......... .......... .......... .......... .......... 74% 10.8M 6s
198500K .......... .......... .......... .......... .......... 74% 12.4M 6s
198550K .......... .......... .......... .......... .......... 74% 10.8M 6s
198600K .......... .......... .......... .......... .......... 74% 11.9M 6s
198650K .......... .......... .......... .......... .......... 74% 8.76M 6s
198700K .......... .......... .......... .......... .......... 74% 5.48M 6s
198750K .......... .......... .......... .......... .......... 74% 53.7M 6s
198800K .......... .......... .......... .......... .......... 74% 9.08M 6s
198850K .......... .......... .......... .......... .......... 74% 7.15M 6s
198900K .......... .......... .......... .......... .......... 74% 8.33M 6s
198950K .......... .......... .......... .......... .......... 74% 7.45M 6s
199000K .......... .......... .......... .......... .......... 74% 9.14M 6s
199050K .......... .......... .......... .......... .......... 74% 11.4M 6s
199100K .......... .......... .......... .......... .......... 75% 6.18M 6s
199150K .......... .......... .......... .......... .......... 75% 10.7M 6s
199200K .......... .......... .......... .......... .......... 75% 8.98M 6s
199250K .......... .......... .......... .......... .......... 75% 6.37M 6s
199300K .......... .......... .......... .......... .......... 75% 9.92M 6s
199350K .......... .......... .......... .......... .......... 75% 6.01M 6s
199400K .......... .......... .......... .......... .......... 75% 11.1M 6s
199450K .......... .......... .......... .......... .......... 75% 9.52M 6s
199500K .......... .......... .......... .......... .......... 75% 10.4M 6s
199550K .......... .......... .......... .......... .......... 75% 11.7M 6s
199600K .......... .......... .......... .......... .......... 75% 9.90M 6s
199650K .......... .......... .......... .......... .......... 75% 14.2M 6s
199700K .......... .......... .......... .......... .......... 75% 8.02M 6s
199750K .......... .......... .......... .......... .......... 75% 12.8M 6s
199800K .......... .......... .......... .......... .......... 75% 12.3M 6s
199850K .......... .......... .......... .......... .......... 75% 10.3M 6s
199900K .......... .......... .......... .......... .......... 75% 14.4M 6s
199950K .......... .......... .......... .......... .......... 75% 14.2M 6s
200000K .......... .......... .......... .......... .......... 75% 13.0M 6s
200050K .......... .......... .......... .......... .......... 75% 13.5M 6s
200100K .......... .......... .......... .......... .......... 75% 10.1M 6s
200150K .......... .......... .......... .......... .......... 75% 13.6M 6s
200200K .......... .......... .......... .......... .......... 75% 10.8M 6s
200250K .......... .......... .......... .......... .......... 75% 12.5M 6s
200300K .......... .......... .......... .......... .......... 75% 12.3M 6s
200350K .......... .......... .......... .......... .......... 75% 14.6M 6s
200400K .......... .......... .......... .......... .......... 75% 12.8M 6s
200450K .......... .......... .......... .......... .......... 75% 14.0M 6s
200500K .......... .......... .......... .......... .......... 75% 12.9M 6s
200550K .......... .......... .......... .......... .......... 75% 13.3M 6s
200600K .......... .......... .......... .......... .......... 75% 8.56M 6s
200650K .......... .......... .......... .......... .......... 75% 15.5M 6s
200700K .......... .......... .......... .......... .......... 75% 11.9M 6s
200750K .......... .......... .......... .......... .......... 75% 11.9M 6s
200800K .......... .......... .......... .......... .......... 75% 18.2M 6s
200850K .......... .......... .......... .......... .......... 75% 12.2M 6s
200900K .......... .......... .......... .......... .......... 75% 20.9M 6s
200950K .......... .......... .......... .......... .......... 75% 11.2M 6s
201000K .......... .......... .......... .......... .......... 75% 21.9M 6s
201050K .......... .......... .......... .......... .......... 75% 12.8M 6s
201100K .......... .......... .......... .......... .......... 75% 13.0M 6s
201150K .......... .......... .......... .......... .......... 75% 18.1M 6s
201200K .......... .......... .......... .......... .......... 75% 11.3M 6s
201250K .......... .......... .......... .......... .......... 75% 12.1M 6s
201300K .......... .......... .......... .......... .......... 75% 15.9M 6s
201350K .......... .......... .......... .......... .......... 75% 13.7M 6s
201400K .......... .......... .......... .......... .......... 75% 12.0M 6s
201450K .......... .......... .......... .......... .......... 75% 14.2M 6s
201500K .......... .......... .......... .......... .......... 75% 20.5M 6s
201550K .......... .......... .......... .......... .......... 75% 17.9M 6s
201600K .......... .......... .......... .......... .......... 75% 13.1M 6s
201650K .......... .......... .......... .......... .......... 75% 12.1M 6s
201700K .......... .......... .......... .......... .......... 75% 18.9M 6s
201750K .......... .......... .......... .......... .......... 76% 16.9M 6s
201800K .......... .......... .......... .......... .......... 76% 11.5M 6s
201850K .......... .......... .......... .......... .......... 76% 12.2M 6s
201900K .......... .......... .......... .......... .......... 76% 24.3M 5s
201950K .......... .......... .......... .......... .......... 76% 19.7M 5s
202000K .......... .......... .......... .......... .......... 76% 15.0M 5s
202050K .......... .......... .......... .......... .......... 76% 12.4M 5s
202100K .......... .......... .......... .......... .......... 76% 16.2M 5s
202150K .......... .......... .......... .......... .......... 76% 23.4M 5s
202200K .......... .......... .......... .......... .......... 76% 12.1M 5s
202250K .......... .......... .......... .......... .......... 76% 14.4M 5s
202300K .......... .......... .......... .......... .......... 76% 17.8M 5s
202350K .......... .......... .......... .......... .......... 76% 13.3M 5s
202400K .......... .......... .......... .......... .......... 76% 21.2M 5s
202450K .......... .......... .......... .......... .......... 76% 13.0M 5s
202500K .......... .......... .......... .......... .......... 76% 15.2M 5s
202550K .......... .......... .......... .......... .......... 76% 15.5M 5s
202600K .......... .......... .......... .......... .......... 76% 31.5M 5s
202650K .......... .......... .......... .......... .......... 76% 15.4M 5s
202700K .......... .......... .......... .......... .......... 76% 26.7M 5s
202750K .......... .......... .......... .......... .......... 76% 11.3M 5s
202800K .......... .......... .......... .......... .......... 76% 18.0M 5s
202850K .......... .......... .......... .......... .......... 76% 16.3M 5s
202900K .......... .......... .......... .......... .......... 76% 14.9M 5s
202950K .......... .......... .......... .......... .......... 76% 12.8M 5s
203000K .......... .......... .......... .......... .......... 76% 28.7M 5s
203050K .......... .......... .......... .......... .......... 76% 16.0M 5s
203100K .......... .......... .......... .......... .......... 76% 28.9M 5s
203150K .......... .......... .......... .......... .......... 76% 12.6M 5s
203200K .......... .......... .......... .......... .......... 76% 15.8M 5s
203250K .......... .......... .......... .......... .......... 76% 38.9M 5s
203300K .......... .......... .......... .......... .......... 76% 13.4M 5s
203350K .......... .......... .......... .......... .......... 76% 39.1M 5s
203400K .......... .......... .......... .......... .......... 76% 17.6M 5s
203450K .......... .......... .......... .......... .......... 76% 22.8M 5s
203500K .......... .......... .......... .......... .......... 76% 26.1M 5s
203550K .......... .......... .......... .......... .......... 76% 15.8M 5s
203600K .......... .......... .......... .......... .......... 76% 35.9M 5s
203650K .......... .......... .......... .......... .......... 76% 17.3M 5s
203700K .......... .......... .......... .......... .......... 76% 24.2M 5s
203750K .......... .......... .......... .......... .......... 76% 14.3M 5s
203800K .......... .......... .......... .......... .......... 76% 18.0M 5s
203850K .......... .......... .......... .......... .......... 76% 28.7M 5s
203900K .......... .......... .......... .......... .......... 76% 26.4M 5s
203950K .......... .......... .......... .......... .......... 76% 20.1M 5s
204000K .......... .......... .......... .......... .......... 76% 14.9M 5s
204050K .......... .......... .......... .......... .......... 76% 30.8M 5s
204100K .......... .......... .......... .......... .......... 76% 20.5M 5s
204150K .......... .......... .......... .......... .......... 76% 19.3M 5s
204200K .......... .......... .......... .......... .......... 76% 34.9M 5s
204250K .......... .......... .......... .......... .......... 76% 15.5M 5s
204300K .......... .......... .......... .......... .......... 76% 22.9M 5s
204350K .......... .......... .......... .......... .......... 76% 18.7M 5s
204400K .......... .......... .......... .......... .......... 77% 15.7M 5s
204450K .......... .......... .......... .......... .......... 77% 43.6M 5s
204500K .......... .......... .......... .......... .......... 77% 15.1M 5s
204550K .......... .......... .......... .......... .......... 77% 35.5M 5s
204600K .......... .......... .......... .......... .......... 77% 13.4M 5s
204650K .......... .......... .......... .......... .......... 77% 57.6M 5s
204700K .......... .......... .......... .......... .......... 77% 11.7M 5s
204750K .......... .......... .......... .......... .......... 77% 103M 5s
204800K .......... .......... .......... .......... .......... 77% 13.5M 5s
204850K .......... .......... .......... .......... .......... 77% 67.6M 5s
204900K .......... .......... .......... .......... .......... 77% 13.8M 5s
204950K .......... .......... .......... .......... .......... 77% 69.4M 5s
205000K .......... .......... .......... .......... .......... 77% 14.4M 5s
205050K .......... .......... .......... .......... .......... 77% 110M 5s
205100K .......... .......... .......... .......... .......... 77% 12.7M 5s
205150K .......... .......... .......... .......... .......... 77% 92.9M 5s
205200K .......... .......... .......... .......... .......... 77% 19.4M 5s
205250K .......... .......... .......... .......... .......... 77% 32.6M 5s
205300K .......... .......... .......... .......... .......... 77% 12.3M 5s
205350K .......... .......... .......... .......... .......... 77% 18.4M 5s
205400K .......... .......... .......... .......... .......... 77% 35.9M 5s
205450K .......... .......... .......... .......... .......... 77% 14.7M 5s
205500K .......... .......... .......... .......... .......... 77% 72.2M 5s
205550K .......... .......... .......... .......... .......... 77% 17.8M 5s
205600K .......... .......... .......... .......... .......... 77% 26.5M 5s
205650K .......... .......... .......... .......... .......... 77% 16.2M 5s
205700K .......... .......... .......... .......... .......... 77% 45.4M 5s
205750K .......... .......... .......... .......... .......... 77% 15.5M 5s
205800K .......... .......... .......... .......... .......... 77% 41.6M 5s
205850K .......... .......... .......... .......... .......... 77% 16.5M 5s
205900K .......... .......... .......... .......... .......... 77% 39.3M 5s
205950K .......... .......... .......... .......... .......... 77% 18.9M 5s
206000K .......... .......... .......... .......... .......... 77% 30.8M 5s
206050K .......... .......... .......... .......... .......... 77% 30.4M 5s
206100K .......... .......... .......... .......... .......... 77% 18.4M 5s
206150K .......... .......... .......... .......... .......... 77% 42.9M 5s
206200K .......... .......... .......... .......... .......... 77% 16.6M 5s
206250K .......... .......... .......... .......... .......... 77% 34.1M 5s
206300K .......... .......... .......... .......... .......... 77% 16.3M 5s
206350K .......... .......... .......... .......... .......... 77% 15.4M 5s
206400K .......... .......... .......... .......... .......... 77% 50.6M 5s
206450K .......... .......... .......... .......... .......... 77% 11.5M 5s
206500K .......... .......... .......... .......... .......... 77% 71.6M 5s
206550K .......... .......... .......... .......... .......... 77% 33.0M 5s
206600K .......... .......... .......... .......... .......... 77% 18.5M 5s
206650K .......... .......... .......... .......... .......... 77% 32.4M 5s
206700K .......... .......... .......... .......... .......... 77% 5.79M 5s
206750K .......... .......... .......... .......... .......... 77% 40.2M 5s
206800K .......... .......... .......... .......... .......... 77% 217M 5s
206850K .......... .......... .......... .......... .......... 77% 227M 5s
206900K .......... .......... .......... .......... .......... 77% 20.6M 5s
206950K .......... .......... .......... .......... .......... 77% 17.1M 5s
207000K .......... .......... .......... .......... .......... 77% 23.0M 5s
207050K .......... .......... .......... .......... .......... 78% 15.8M 5s
207100K .......... .......... .......... .......... .......... 78% 15.5M 5s
207150K .......... .......... .......... .......... .......... 78% 24.2M 5s
207200K .......... .......... .......... .......... .......... 78% 17.0M 5s
207250K .......... .......... .......... .......... .......... 78% 12.6M 5s
207300K .......... .......... .......... .......... .......... 78% 17.6M 5s
207350K .......... .......... .......... .......... .......... 78% 16.8M 5s
207400K .......... .......... .......... .......... .......... 78% 14.2M 5s
207450K .......... .......... .......... .......... .......... 78% 22.8M 5s
207500K .......... .......... .......... .......... .......... 78% 11.8M 5s
207550K .......... .......... .......... .......... .......... 78% 29.3M 5s
207600K .......... .......... .......... .......... .......... 78% 12.7M 5s
207650K .......... .......... .......... .......... .......... 78% 45.3M 5s
207700K .......... .......... .......... .......... .......... 78% 11.9M 5s
207750K .......... .......... .......... .......... .......... 78% 12.2M 5s
207800K .......... .......... .......... .......... .......... 78% 38.7M 5s
207850K .......... .......... .......... .......... .......... 78% 12.7M 5s
207900K .......... .......... .......... .......... .......... 78% 49.7M 5s
207950K .......... .......... .......... .......... .......... 78% 13.1M 5s
208000K .......... .......... .......... .......... .......... 78% 15.7M 5s
208050K .......... .......... .......... .......... .......... 78% 27.0M 5s
208100K .......... .......... .......... .......... .......... 78% 16.5M 5s
208150K .......... .......... .......... .......... .......... 78% 54.0M 5s
208200K .......... .......... .......... .......... .......... 78% 11.6M 5s
208250K .......... .......... .......... .......... .......... 78% 43.0M 5s
208300K .......... .......... .......... .......... .......... 78% 18.1M 5s
208350K .......... .......... .......... .......... .......... 78% 18.5M 5s
208400K .......... .......... .......... .......... .......... 78% 26.4M 5s
208450K .......... .......... .......... .......... .......... 78% 14.0M 5s
208500K .......... .......... .......... .......... .......... 78% 93.4M 5s
208550K .......... .......... .......... .......... .......... 78% 12.6M 5s
208600K .......... .......... .......... .......... .......... 78% 18.8M 5s
208650K .......... .......... .......... .......... .......... 78% 29.8M 5s
208700K .......... .......... .......... .......... .......... 78% 13.1M 5s
208750K .......... .......... .......... .......... .......... 78% 133M 5s
208800K .......... .......... .......... .......... .......... 78% 12.4M 5s
208850K .......... .......... .......... .......... .......... 78% 45.1M 5s
208900K .......... .......... .......... .......... .......... 78% 15.0M 5s
208950K .......... .......... .......... .......... .......... 78% 12.6M 5s
209000K .......... .......... .......... .......... .......... 78% 56.6M 5s
209050K .......... .......... .......... .......... .......... 78% 14.6M 5s
209100K .......... .......... .......... .......... .......... 78% 32.0M 5s
209150K .......... .......... .......... .......... .......... 78% 13.6M 5s
209200K .......... .......... .......... .......... .......... 78% 19.3M 5s
209250K .......... .......... .......... .......... .......... 78% 38.1M 5s
209300K .......... .......... .......... .......... .......... 78% 21.1M 5s
209350K .......... .......... .......... .......... .......... 78% 16.3M 5s
209400K .......... .......... .......... .......... .......... 78% 19.6M 5s
209450K .......... .......... .......... .......... .......... 78% 16.8M 5s
209500K .......... .......... .......... .......... .......... 78% 36.8M 5s
209550K .......... .......... .......... .......... .......... 78% 24.4M 5s
209600K .......... .......... .......... .......... .......... 78% 19.0M 5s
209650K .......... .......... .......... .......... .......... 78% 13.2M 5s
209700K .......... .......... .......... .......... .......... 78% 62.5M 5s
209750K .......... .......... .......... .......... .......... 79% 15.7M 5s
209800K .......... .......... .......... .......... .......... 79% 43.2M 5s
209850K .......... .......... .......... .......... .......... 79% 16.8M 5s
209900K .......... .......... .......... .......... .......... 79% 26.9M 5s
209950K .......... .......... .......... .......... .......... 79% 17.9M 5s
210000K .......... .......... .......... .......... .......... 79% 26.0M 5s
210050K .......... .......... .......... .......... .......... 79% 21.3M 5s
210100K .......... .......... .......... .......... .......... 79% 25.5M 5s
210150K .......... .......... .......... .......... .......... 79% 17.3M 5s
210200K .......... .......... .......... .......... .......... 79% 18.8M 5s
210250K .......... .......... .......... .......... .......... 79% 34.4M 5s
210300K .......... .......... .......... .......... .......... 79% 29.3M 5s
210350K .......... .......... .......... .......... .......... 79% 18.0M 5s
210400K .......... .......... .......... .......... .......... 79% 7.71M 5s
210450K .......... .......... .......... .......... .......... 79% 28.5M 5s
210500K .......... .......... .......... .......... .......... 79% 97.7M 5s
210550K .......... .......... .......... .......... .......... 79% 14.9M 5s
210600K .......... .......... .......... .......... .......... 79% 65.0M 5s
210650K .......... .......... .......... .......... .......... 79% 12.6M 5s
210700K .......... .......... .......... .......... .......... 79% 12.9M 5s
210750K .......... .......... .......... .......... .......... 79% 71.0M 5s
210800K .......... .......... .......... .......... .......... 79% 13.2M 5s
210850K .......... .......... .......... .......... .......... 79% 12.9M 5s
210900K .......... .......... .......... .......... .......... 79% 18.4M 5s
210950K .......... .......... .......... .......... .......... 79% 11.5M 5s
211000K .......... .......... .......... .......... .......... 79% 24.9M 5s
211050K .......... .......... .......... .......... .......... 79% 14.1M 5s
211100K .......... .......... .......... .......... .......... 79% 12.3M 5s
211150K .......... .......... .......... .......... .......... 79% 52.5M 5s
211200K .......... .......... .......... .......... .......... 79% 11.9M 5s
211250K .......... .......... .......... .......... .......... 79% 14.9M 5s
211300K .......... .......... .......... .......... .......... 79% 23.9M 5s
211350K .......... .......... .......... .......... .......... 79% 17.0M 5s
211400K .......... .......... .......... .......... .......... 79% 15.9M 5s
211450K .......... .......... .......... .......... .......... 79% 28.3M 5s
211500K .......... .......... .......... .......... .......... 79% 15.3M 5s
211550K .......... .......... .......... .......... .......... 79% 15.8M 5s
211600K .......... .......... .......... .......... .......... 79% 12.9M 5s
211650K .......... .......... .......... .......... .......... 79% 36.5M 5s
211700K .......... .......... .......... .......... .......... 79% 12.2M 5s
211750K .......... .......... .......... .......... .......... 79% 13.1M 5s
211800K .......... .......... .......... .......... .......... 79% 59.8M 5s
211850K .......... .......... .......... .......... .......... 79% 15.3M 5s
211900K .......... .......... .......... .......... .......... 79% 23.9M 5s
211950K .......... .......... .......... .......... .......... 79% 22.9M 5s
212000K .......... .......... .......... .......... .......... 79% 12.6M 5s
212050K .......... .......... .......... .......... .......... 79% 24.7M 5s
212100K .......... .......... .......... .......... .......... 79% 17.1M 5s
212150K .......... .......... .......... .......... .......... 79% 17.5M 5s
212200K .......... .......... .......... .......... .......... 79% 15.2M 5s
212250K .......... .......... .......... .......... .......... 79% 14.1M 5s
212300K .......... .......... .......... .......... .......... 79% 28.5M 5s
212350K .......... .......... .......... .......... .......... 79% 10.8M 5s
212400K .......... .......... .......... .......... .......... 80% 35.6M 4s
212450K .......... .......... .......... .......... .......... 80% 13.3M 4s
212500K .......... .......... .......... .......... .......... 80% 21.7M 4s
212550K .......... .......... .......... .......... .......... 80% 25.2M 4s
212600K .......... .......... .......... .......... .......... 80% 12.2M 4s
212650K .......... .......... .......... .......... .......... 80% 19.3M 4s
212700K .......... .......... .......... .......... .......... 80% 19.9M 4s
212750K .......... .......... .......... .......... .......... 80% 15.5M 4s
212800K .......... .......... .......... .......... .......... 80% 27.2M 4s
212850K .......... .......... .......... .......... .......... 80% 14.5M 4s
212900K .......... .......... .......... .......... .......... 80% 18.5M 4s
212950K .......... .......... .......... .......... .......... 80% 31.0M 4s
213000K .......... .......... .......... .......... .......... 80% 19.2M 4s
213050K .......... .......... .......... .......... .......... 80% 24.4M 4s
213100K .......... .......... .......... .......... .......... 80% 14.6M 4s
213150K .......... .......... .......... .......... .......... 80% 34.4M 4s
213200K .......... .......... .......... .......... .......... 80% 12.3M 4s
213250K .......... .......... .......... .......... .......... 80% 15.1M 4s
213300K .......... .......... .......... .......... .......... 80% 25.7M 4s
213350K .......... .......... .......... .......... .......... 80% 17.0M 4s
213400K .......... .......... .......... .......... .......... 80% 21.1M 4s
213450K .......... .......... .......... .......... .......... 80% 20.9M 4s
213500K .......... .......... .......... .......... .......... 80% 21.3M 4s
213550K .......... .......... .......... .......... .......... 80% 14.5M 4s
213600K .......... .......... .......... .......... .......... 80% 16.2M 4s
213650K .......... .......... .......... .......... .......... 80% 27.6M 4s
213700K .......... .......... .......... .......... .......... 80% 14.3M 4s
213750K .......... .......... .......... .......... .......... 80% 36.2M 4s
213800K .......... .......... .......... .......... .......... 80% 12.8M 4s
213850K .......... .......... .......... .......... .......... 80% 5.72M 4s
213900K .......... .......... .......... .......... .......... 80% 70.2M 4s
213950K .......... .......... .......... .......... .......... 80% 64.3M 4s
214000K .......... .......... .......... .......... .......... 80% 17.7M 4s
214050K .......... .......... .......... .......... .......... 80% 34.7M 4s
214100K .......... .......... .......... .......... .......... 80% 12.6M 4s
214150K .......... .......... .......... .......... .......... 80% 13.7M 4s
214200K .......... .......... .......... .......... .......... 80% 14.5M 4s
214250K .......... .......... .......... .......... .......... 80% 14.0M 4s
214300K .......... .......... .......... .......... .......... 80% 44.0M 4s
214350K .......... .......... .......... .......... .......... 80% 12.5M 4s
214400K .......... .......... .......... .......... .......... 80% 13.1M 4s
214450K .......... .......... .......... .......... .......... 80% 13.9M 4s
214500K .......... .......... .......... .......... .......... 80% 30.8M 4s
214550K .......... .......... .......... .......... .......... 80% 13.9M 4s
214600K .......... .......... .......... .......... .......... 80% 10.8M 4s
214650K .......... .......... .......... .......... .......... 80% 103M 4s
214700K .......... .......... .......... .......... .......... 80% 14.0M 4s
214750K .......... .......... .......... .......... .......... 80% 11.7M 4s
214800K .......... .......... .......... .......... .......... 80% 14.5M 4s
214850K .......... .......... .......... .......... .......... 80% 31.8M 4s
214900K .......... .......... .......... .......... .......... 80% 5.88M 4s
214950K .......... .......... .......... .......... .......... 80% 191M 4s
215000K .......... .......... .......... .......... .......... 80% 14.6M 4s
215050K .......... .......... .......... .......... .......... 81% 13.5M 4s
215100K .......... .......... .......... .......... .......... 81% 12.4M 4s
215150K .......... .......... .......... .......... .......... 81% 46.9M 4s
215200K .......... .......... .......... .......... .......... 81% 6.91M 4s
215250K .......... .......... .......... .......... .......... 81% 12.4M 4s
215300K .......... .......... .......... .......... .......... 81% 43.1M 4s
215350K .......... .......... .......... .......... .......... 81% 10.4M 4s
215400K .......... .......... .......... .......... .......... 81% 13.4M 4s
215450K .......... .......... .......... .......... .......... 81% 11.4M 4s
215500K .......... .......... .......... .......... .......... 81% 13.3M 4s
215550K .......... .......... .......... .......... .......... 81% 11.6M 4s
215600K .......... .......... .......... .......... .......... 81% 13.5M 4s
215650K .......... .......... .......... .......... .......... 81% 13.1M 4s
215700K .......... .......... .......... .......... .......... 81% 11.2M 4s
215750K .......... .......... .......... .......... .......... 81% 15.1M 4s
215800K .......... .......... .......... .......... .......... 81% 12.6M 4s
215850K .......... .......... .......... .......... .......... 81% 12.1M 4s
215900K .......... .......... .......... .......... .......... 81% 34.1M 4s
215950K .......... .......... .......... .......... .......... 81% 12.6M 4s
216000K .......... .......... .......... .......... .......... 81% 12.1M 4s
216050K .......... .......... .......... .......... .......... 81% 12.9M 4s
216100K .......... .......... .......... .......... .......... 81% 14.7M 4s
216150K .......... .......... .......... .......... .......... 81% 53.7M 4s
216200K .......... .......... .......... .......... .......... 81% 12.9M 4s
216250K .......... .......... .......... .......... .......... 81% 12.6M 4s
216300K .......... .......... .......... .......... .......... 81% 15.6M 4s
216350K .......... .......... .......... .......... .......... 81% 9.89M 4s
216400K .......... .......... .......... .......... .......... 81% 139M 4s
216450K .......... .......... .......... .......... .......... 81% 13.5M 4s
216500K .......... .......... .......... .......... .......... 81% 13.4M 4s
216550K .......... .......... .......... .......... .......... 81% 13.6M 4s
216600K .......... .......... .......... .......... .......... 81% 18.1M 4s
216650K .......... .......... .......... .......... .......... 81% 19.0M 4s
216700K .......... .......... .......... .......... .......... 81% 14.2M 4s
216750K .......... .......... .......... .......... .......... 81% 13.4M 4s
216800K .......... .......... .......... .......... .......... 81% 29.5M 4s
216850K .......... .......... .......... .......... .......... 81% 14.0M 4s
216900K .......... .......... .......... .......... .......... 81% 21.8M 4s
216950K .......... .......... .......... .......... .......... 81% 9.16M 4s
217000K .......... .......... .......... .......... .......... 81% 114M 4s
217050K .......... .......... .......... .......... .......... 81% 15.8M 4s
217100K .......... .......... .......... .......... .......... 81% 13.4M 4s
217150K .......... .......... .......... .......... .......... 81% 23.1M 4s
217200K .......... .......... .......... .......... .......... 81% 13.3M 4s
217250K .......... .......... .......... .......... .......... 81% 29.2M 4s
217300K .......... .......... .......... .......... .......... 81% 14.0M 4s
217350K .......... .......... .......... .......... .......... 81% 14.7M 4s
217400K .......... .......... .......... .......... .......... 81% 49.9M 4s
217450K .......... .......... .......... .......... .......... 81% 12.1M 4s
217500K .......... .......... .......... .......... .......... 81% 15.4M 4s
217550K .......... .......... .......... .......... .......... 81% 21.2M 4s
217600K .......... .......... .......... .......... .......... 81% 16.9M 4s
217650K .......... .......... .......... .......... .......... 81% 13.0M 4s
217700K .......... .......... .......... .......... .......... 82% 27.5M 4s
217750K .......... .......... .......... .......... .......... 82% 12.7M 4s
217800K .......... .......... .......... .......... .......... 82% 13.7M 4s
217850K .......... .......... .......... .......... .......... 82% 19.0M 4s
217900K .......... .......... .......... .......... .......... 82% 31.4M 4s
217950K .......... .......... .......... .......... .......... 82% 11.8M 4s
218000K .......... .......... .......... .......... .......... 82% 16.2M 4s
218050K .......... .......... .......... .......... .......... 82% 42.1M 4s
218100K .......... .......... .......... .......... .......... 82% 13.7M 4s
218150K .......... .......... .......... .......... .......... 82% 19.5M 4s
218200K .......... .......... .......... .......... .......... 82% 12.3M 4s
218250K .......... .......... .......... .......... .......... 82% 35.7M 4s
218300K .......... .......... .......... .......... .......... 82% 17.0M 4s
218350K .......... .......... .......... .......... .......... 82% 11.8M 4s
218400K .......... .......... .......... .......... .......... 82% 16.8M 4s
218450K .......... .......... .......... .......... .......... 82% 23.9M 4s
218500K .......... .......... .......... .......... .......... 82% 14.7M 4s
218550K .......... .......... .......... .......... .......... 82% 19.4M 4s
218600K .......... .......... .......... .......... .......... 82% 23.9M 4s
218650K .......... .......... .......... .......... .......... 82% 13.9M 4s
218700K .......... .......... .......... .......... .......... 82% 31.5M 4s
218750K .......... .......... .......... .......... .......... 82% 11.9M 4s
218800K .......... .......... .......... .......... .......... 82% 32.5M 4s
218850K .......... .......... .......... .......... .......... 82% 12.9M 4s
218900K .......... .......... .......... .......... .......... 82% 6.54M 4s
218950K .......... .......... .......... .......... .......... 82% 39.6M 4s
219000K .......... .......... .......... .......... .......... 82% 89.2M 4s
219050K .......... .......... .......... .......... .......... 82% 21.1M 4s
219100K .......... .......... .......... .......... .......... 82% 14.6M 4s
219150K .......... .......... .......... .......... .......... 82% 35.9M 4s
219200K .......... .......... .......... .......... .......... 82% 13.5M 4s
219250K .......... .......... .......... .......... .......... 82% 21.4M 4s
219300K .......... .......... .......... .......... .......... 82% 15.6M 4s
219350K .......... .......... .......... .......... .......... 82% 12.3M 4s
219400K .......... .......... .......... .......... .......... 82% 16.7M 4s
219450K .......... .......... .......... .......... .......... 82% 12.9M 4s
219500K .......... .......... .......... .......... .......... 82% 70.6M 4s
219550K .......... .......... .......... .......... .......... 82% 5.09M 4s
219600K .......... .......... .......... .......... .......... 82% 130M 4s
219650K .......... .......... .......... .......... .......... 82% 66.3M 4s
219700K .......... .......... .......... .......... .......... 82% 10.9M 4s
219750K .......... .......... .......... .......... .......... 82% 12.4M 4s
219800K .......... .......... .......... .......... .......... 82% 12.4M 4s
219850K .......... .......... .......... .......... .......... 82% 13.7M 4s
219900K .......... .......... .......... .......... .......... 82% 12.9M 4s
219950K .......... .......... .......... .......... .......... 82% 4.67M 4s
220000K .......... .......... .......... .......... .......... 82% 35.0M 4s
220050K .......... .......... .......... .......... .......... 82% 9.32M 4s
220100K .......... .......... .......... .......... .......... 82% 7.08M 4s
220150K .......... .......... .......... .......... .......... 82% 7.90M 4s
220200K .......... .......... .......... .......... .......... 82% 7.00M 4s
220250K .......... .......... .......... .......... .......... 82% 7.90M 4s
220300K .......... .......... .......... .......... .......... 82% 8.52M 4s
220350K .......... .......... .......... .......... .......... 83% 6.39M 4s
220400K .......... .......... .......... .......... .......... 83% 10.4M 4s
220450K .......... .......... .......... .......... .......... 83% 7.75M 4s
220500K .......... .......... .......... .......... .......... 83% 9.57M 4s
220550K .......... .......... .......... .......... .......... 83% 7.33M 4s
220600K .......... .......... .......... .......... .......... 83% 4.70M 4s
220650K .......... .......... .......... .......... .......... 83% 9.86M 4s
220700K .......... .......... .......... .......... .......... 83% 7.72M 4s
220750K .......... .......... .......... .......... .......... 83% 7.37M 4s
220800K .......... .......... .......... .......... .......... 83% 8.36M 4s
220850K .......... .......... .......... .......... .......... 83% 6.34M 4s
220900K .......... .......... .......... .......... .......... 83% 7.50M 4s
220950K .......... .......... .......... .......... .......... 83% 6.72M 4s
221000K .......... .......... .......... .......... .......... 83% 8.31M 4s
221050K .......... .......... .......... .......... .......... 83% 8.12M 4s
221100K .......... .......... .......... .......... .......... 83% 6.91M 4s
221150K .......... .......... .......... .......... .......... 83% 7.03M 4s
221200K .......... .......... .......... .......... .......... 83% 4.42M 4s
221250K .......... .......... .......... .......... .......... 83% 11.5M 4s
221300K .......... .......... .......... .......... .......... 83% 6.15M 4s
221350K .......... .......... .......... .......... .......... 83% 6.52M 4s
221400K .......... .......... .......... .......... .......... 83% 5.64M 4s
221450K .......... .......... .......... .......... .......... 83% 6.68M 4s
221500K .......... .......... .......... .......... .......... 83% 7.29M 4s
221550K .......... .......... .......... .......... .......... 83% 6.44M 4s
221600K .......... .......... .......... .......... .......... 83% 7.06M 4s
221650K .......... .......... .......... .......... .......... 83% 5.54M 4s
221700K .......... .......... .......... .......... .......... 83% 5.30M 4s
221750K .......... .......... .......... .......... .......... 83% 9.29M 4s
221800K .......... .......... .......... .......... .......... 83% 6.71M 4s
221850K .......... .......... .......... .......... .......... 83% 6.32M 4s
221900K .......... .......... .......... .......... .......... 83% 6.04M 4s
221950K .......... .......... .......... .......... .......... 83% 9.19M 4s
222000K .......... .......... .......... .......... .......... 83% 8.35M 4s
222050K .......... .......... .......... .......... .......... 83% 9.29M 4s
222100K .......... .......... .......... .......... .......... 83% 8.12M 4s
222150K .......... .......... .......... .......... .......... 83% 8.26M 4s
222200K .......... .......... .......... .......... .......... 83% 8.35M 4s
222250K .......... .......... .......... .......... .......... 83% 8.44M 4s
222300K .......... .......... .......... .......... .......... 83% 12.5M 4s
222350K .......... .......... .......... .......... .......... 83% 7.09M 4s
222400K .......... .......... .......... .......... .......... 83% 10.7M 4s
222450K .......... .......... .......... .......... .......... 83% 9.60M 4s
222500K .......... .......... .......... .......... .......... 83% 12.4M 4s
222550K .......... .......... .......... .......... .......... 83% 13.5M 4s
222600K .......... .......... .......... .......... .......... 83% 8.08M 4s
222650K .......... .......... .......... .......... .......... 83% 11.7M 4s
222700K .......... .......... .......... .......... .......... 83% 11.8M 4s
222750K .......... .......... .......... .......... .......... 83% 14.6M 4s
222800K .......... .......... .......... .......... .......... 83% 12.5M 4s
222850K .......... .......... .......... .......... .......... 83% 13.0M 4s
222900K .......... .......... .......... .......... .......... 83% 10.6M 4s
222950K .......... .......... .......... .......... .......... 83% 12.2M 4s
223000K .......... .......... .......... .......... .......... 84% 12.6M 4s
223050K .......... .......... .......... .......... .......... 84% 11.6M 4s
223100K .......... .......... .......... .......... .......... 84% 13.4M 4s
223150K .......... .......... .......... .......... .......... 84% 11.0M 4s
223200K .......... .......... .......... .......... .......... 84% 11.9M 4s
223250K .......... .......... .......... .......... .......... 84% 14.5M 4s
223300K .......... .......... .......... .......... .......... 84% 10.2M 4s
223350K .......... .......... .......... .......... .......... 84% 15.5M 4s
223400K .......... .......... .......... .......... .......... 84% 12.6M 4s
223450K .......... .......... .......... .......... .......... 84% 13.3M 4s
223500K .......... .......... .......... .......... .......... 84% 13.3M 4s
223550K .......... .......... .......... .......... .......... 84% 11.8M 4s
223600K .......... .......... .......... .......... .......... 84% 25.6M 4s
223650K .......... .......... .......... .......... .......... 84% 12.3M 4s
223700K .......... .......... .......... .......... .......... 84% 13.4M 4s
223750K .......... .......... .......... .......... .......... 84% 12.4M 4s
223800K .......... .......... .......... .......... .......... 84% 15.5M 4s
223850K .......... .......... .......... .......... .......... 84% 10.1M 4s
223900K .......... .......... .......... .......... .......... 84% 20.6M 4s
223950K .......... .......... .......... .......... .......... 84% 12.9M 4s
224000K .......... .......... .......... .......... .......... 84% 13.2M 4s
224050K .......... .......... .......... .......... .......... 84% 11.5M 3s
224100K .......... .......... .......... .......... .......... 84% 12.4M 3s
224150K .......... .......... .......... .......... .......... 84% 7.08M 3s
224200K .......... .......... .......... .......... .......... 84% 124M 3s
224250K .......... .......... .......... .......... .......... 84% 12.5M 3s
224300K .......... .......... .......... .......... .......... 84% 13.8M 3s
224350K .......... .......... .......... .......... .......... 84% 10.4M 3s
224400K .......... .......... .......... .......... .......... 84% 15.4M 3s
224450K .......... .......... .......... .......... .......... 84% 10.3M 3s
224500K .......... .......... .......... .......... .......... 84% 13.0M 3s
224550K .......... .......... .......... .......... .......... 84% 13.4M 3s
224600K .......... .......... .......... .......... .......... 84% 11.3M 3s
224650K .......... .......... .......... .......... .......... 84% 13.0M 3s
224700K .......... .......... .......... .......... .......... 84% 10.8M 3s
224750K .......... .......... .......... .......... .......... 84% 13.8M 3s
224800K .......... .......... .......... .......... .......... 84% 13.6M 3s
224850K .......... .......... .......... .......... .......... 84% 11.9M 3s
224900K .......... .......... .......... .......... .......... 84% 13.5M 3s
224950K .......... .......... .......... .......... .......... 84% 11.5M 3s
225000K .......... .......... .......... .......... .......... 84% 9.49M 3s
225050K .......... .......... .......... .......... .......... 84% 13.5M 3s
225100K .......... .......... .......... .......... .......... 84% 18.2M 3s
225150K .......... .......... .......... .......... .......... 84% 12.6M 3s
225200K .......... .......... .......... .......... .......... 84% 12.6M 3s
225250K .......... .......... .......... .......... .......... 84% 17.1M 3s
225300K .......... .......... .......... .......... .......... 84% 20.8M 3s
225350K .......... .......... .......... .......... .......... 84% 10.8M 3s
225400K .......... .......... .......... .......... .......... 84% 14.2M 3s
225450K .......... .......... .......... .......... .......... 84% 9.97M 3s
225500K .......... .......... .......... .......... .......... 84% 19.3M 3s
225550K .......... .......... .......... .......... .......... 84% 18.1M 3s
225600K .......... .......... .......... .......... .......... 84% 15.7M 3s
225650K .......... .......... .......... .......... .......... 85% 14.3M 3s
225700K .......... .......... .......... .......... .......... 85% 12.9M 3s
225750K .......... .......... .......... .......... .......... 85% 11.9M 3s
225800K .......... .......... .......... .......... .......... 85% 32.9M 3s
225850K .......... .......... .......... .......... .......... 85% 12.1M 3s
225900K .......... .......... .......... .......... .......... 85% 5.33M 3s
225950K .......... .......... .......... .......... .......... 85% 110M 3s
226000K .......... .......... .......... .......... .......... 85% 33.8M 3s
226050K .......... .......... .......... .......... .......... 85% 13.2M 3s
226100K .......... .......... .......... .......... .......... 85% 7.30M 3s
226150K .......... .......... .......... .......... .......... 85% 13.9M 3s
226200K .......... .......... .......... .......... .......... 85% 9.18M 3s
226250K .......... .......... .......... .......... .......... 85% 16.4M 3s
226300K .......... .......... .......... .......... .......... 85% 11.8M 3s
226350K .......... .......... .......... .......... .......... 85% 11.6M 3s
226400K .......... .......... .......... .......... .......... 85% 10.2M 3s
226450K .......... .......... .......... .......... .......... 85% 14.7M 3s
226500K .......... .......... .......... .......... .......... 85% 10.4M 3s
226550K .......... .......... .......... .......... .......... 85% 11.5M 3s
226600K .......... .......... .......... .......... .......... 85% 11.6M 3s
226650K .......... .......... .......... .......... .......... 85% 21.9M 3s
226700K .......... .......... .......... .......... .......... 85% 11.2M 3s
226750K .......... .......... .......... .......... .......... 85% 19.4M 3s
226800K .......... .......... .......... .......... .......... 85% 12.4M 3s
226850K .......... .......... .......... .......... .......... 85% 8.84M 3s
226900K .......... .......... .......... .......... .......... 85% 18.2M 3s
226950K .......... .......... .......... .......... .......... 85% 13.2M 3s
227000K .......... .......... .......... .......... .......... 85% 11.7M 3s
227050K .......... .......... .......... .......... .......... 85% 12.0M 3s
227100K .......... .......... .......... .......... .......... 85% 4.91M 3s
227150K .......... .......... .......... .......... .......... 85% 33.2M 3s
227200K .......... .......... .......... .......... .......... 85% 16.3M 3s
227250K .......... .......... .......... .......... .......... 85% 13.3M 3s
227300K .......... .......... .......... .......... .......... 85% 12.5M 3s
227350K .......... .......... .......... .......... .......... 85% 7.74M 3s
227400K .......... .......... .......... .......... .......... 85% 12.3M 3s
227450K .......... .......... .......... .......... .......... 85% 9.06M 3s
227500K .......... .......... .......... .......... .......... 85% 8.52M 3s
227550K .......... .......... .......... .......... .......... 85% 12.3M 3s
227600K .......... .......... .......... .......... .......... 85% 9.33M 3s
227650K .......... .......... .......... .......... .......... 85% 11.2M 3s
227700K .......... .......... .......... .......... .......... 85% 10.3M 3s
227750K .......... .......... .......... .......... .......... 85% 11.6M 3s
227800K .......... .......... .......... .......... .......... 85% 11.9M 3s
227850K .......... .......... .......... .......... .......... 85% 8.49M 3s
227900K .......... .......... .......... .......... .......... 85% 14.7M 3s
227950K .......... .......... .......... .......... .......... 85% 7.69M 3s
228000K .......... .......... .......... .......... .......... 85% 12.5M 3s
228050K .......... .......... .......... .......... .......... 85% 17.5M 3s
228100K .......... .......... .......... .......... .......... 85% 9.84M 3s
228150K .......... .......... .......... .......... .......... 85% 11.8M 3s
228200K .......... .......... .......... .......... .......... 85% 11.4M 3s
228250K .......... .......... .......... .......... .......... 85% 14.4M 3s
228300K .......... .......... .......... .......... .......... 86% 13.7M 3s
228350K .......... .......... .......... .......... .......... 86% 7.74M 3s
228400K .......... .......... .......... .......... .......... 86% 10.9M 3s
228450K .......... .......... .......... .......... .......... 86% 14.8M 3s
228500K .......... .......... .......... .......... .......... 86% 13.6M 3s
228550K .......... .......... .......... .......... .......... 86% 12.5M 3s
228600K .......... .......... .......... .......... .......... 86% 29.8M 3s
228650K .......... .......... .......... .......... .......... 86% 10.4M 3s
228700K .......... .......... .......... .......... .......... 86% 13.7M 3s
228750K .......... .......... .......... .......... .......... 86% 12.7M 3s
228800K .......... .......... .......... .......... .......... 86% 10.8M 3s
228850K .......... .......... .......... .......... .......... 86% 13.6M 3s
228900K .......... .......... .......... .......... .......... 86% 18.5M 3s
228950K .......... .......... .......... .......... .......... 86% 11.3M 3s
229000K .......... .......... .......... .......... .......... 86% 23.3M 3s
229050K .......... .......... .......... .......... .......... 86% 13.5M 3s
229100K .......... .......... .......... .......... .......... 86% 9.93M 3s
229150K .......... .......... .......... .......... .......... 86% 15.5M 3s
229200K .......... .......... .......... .......... .......... 86% 16.6M 3s
229250K .......... .......... .......... .......... .......... 86% 27.5M 3s
229300K .......... .......... .......... .......... .......... 86% 11.4M 3s
229350K .......... .......... .......... .......... .......... 86% 14.0M 3s
229400K .......... .......... .......... .......... .......... 86% 14.5M 3s
229450K .......... .......... .......... .......... .......... 86% 20.3M 3s
229500K .......... .......... .......... .......... .......... 86% 18.4M 3s
229550K .......... .......... .......... .......... .......... 86% 14.4M 3s
229600K .......... .......... .......... .......... .......... 86% 15.2M 3s
229650K .......... .......... .......... .......... .......... 86% 54.6M 3s
229700K .......... .......... .......... .......... .......... 86% 13.6M 3s
229750K .......... .......... .......... .......... .......... 86% 13.5M 3s
229800K .......... .......... .......... .......... .......... 86% 35.0M 3s
229850K .......... .......... .......... .......... .......... 86% 10.4M 3s
229900K .......... .......... .......... .......... .......... 86% 21.1M 3s
229950K .......... .......... .......... .......... .......... 86% 17.0M 3s
230000K .......... .......... .......... .......... .......... 86% 12.8M 3s
230050K .......... .......... .......... .......... .......... 86% 21.3M 3s
230100K .......... .......... .......... .......... .......... 86% 17.1M 3s
230150K .......... .......... .......... .......... .......... 86% 15.8M 3s
230200K .......... .......... .......... .......... .......... 86% 11.4M 3s
230250K .......... .......... .......... .......... .......... 86% 21.5M 3s
230300K .......... .......... .......... .......... .......... 86% 17.0M 3s
230350K .......... .......... .......... .......... .......... 86% 12.7M 3s
230400K .......... .......... .......... .......... .......... 86% 7.66M 3s
230450K .......... .......... .......... .......... .......... 86% 71.2M 3s
230500K .......... .......... .......... .......... .......... 86% 11.3M 3s
230550K .......... .......... .......... .......... .......... 86% 12.5M 3s
230600K .......... .......... .......... .......... .......... 86% 13.1M 3s
230650K .......... .......... .......... .......... .......... 86% 11.4M 3s
230700K .......... .......... .......... .......... .......... 86% 13.5M 3s
230750K .......... .......... .......... .......... .......... 86% 26.7M 3s
230800K .......... .......... .......... .......... .......... 86% 12.8M 3s
230850K .......... .......... .......... .......... .......... 86% 13.6M 3s
230900K .......... .......... .......... .......... .......... 86% 13.2M 3s
230950K .......... .......... .......... .......... .......... 87% 12.7M 3s
231000K .......... .......... .......... .......... .......... 87% 13.6M 3s
231050K .......... .......... .......... .......... .......... 87% 12.2M 3s
231100K .......... .......... .......... .......... .......... 87% 11.9M 3s
231150K .......... .......... .......... .......... .......... 87% 14.1M 3s
231200K .......... .......... .......... .......... .......... 87% 13.5M 3s
231250K .......... .......... .......... .......... .......... 87% 14.0M 3s
231300K .......... .......... .......... .......... .......... 87% 14.3M 3s
231350K .......... .......... .......... .......... .......... 87% 11.4M 3s
231400K .......... .......... .......... .......... .......... 87% 14.4M 3s
231450K .......... .......... .......... .......... .......... 87% 12.7M 3s
231500K .......... .......... .......... .......... .......... 87% 13.6M 3s
231550K .......... .......... .......... .......... .......... 87% 23.9M 3s
231600K .......... .......... .......... .......... .......... 87% 14.5M 3s
231650K .......... .......... .......... .......... .......... 87% 7.91M 3s
231700K .......... .......... .......... .......... .......... 87% 49.6M 3s
231750K .......... .......... .......... .......... .......... 87% 15.9M 3s
231800K .......... .......... .......... .......... .......... 87% 18.1M 3s
231850K .......... .......... .......... .......... .......... 87% 13.3M 3s
231900K .......... .......... .......... .......... .......... 87% 19.6M 3s
231950K .......... .......... .......... .......... .......... 87% 12.6M 3s
232000K .......... .......... .......... .......... .......... 87% 17.1M 3s
232050K .......... .......... .......... .......... .......... 87% 17.4M 3s
232100K .......... .......... .......... .......... .......... 87% 5.12M 3s
232150K .......... .......... .......... .......... .......... 87% 44.2M 3s
232200K .......... .......... .......... .......... .......... 87% 41.8M 3s
232250K .......... .......... .......... .......... .......... 87% 12.4M 3s
232300K .......... .......... .......... .......... .......... 87% 12.4M 3s
232350K .......... .......... .......... .......... .......... 87% 10.3M 3s
232400K .......... .......... .......... .......... .......... 87% 15.1M 3s
232450K .......... .......... .......... .......... .......... 87% 9.38M 3s
232500K .......... .......... .......... .......... .......... 87% 14.0M 3s
232550K .......... .......... .......... .......... .......... 87% 11.1M 3s
232600K .......... .......... .......... .......... .......... 87% 13.4M 3s
232650K .......... .......... .......... .......... .......... 87% 5.80M 3s
232700K .......... .......... .......... .......... .......... 87% 91.0M 3s
232750K .......... .......... .......... .......... .......... 87% 13.5M 3s
232800K .......... .......... .......... .......... .......... 87% 4.48M 3s
232850K .......... .......... .......... .......... .......... 87% 92.1M 3s
232900K .......... .......... .......... .......... .......... 87% 6.92M 3s
232950K .......... .......... .......... .......... .......... 87% 6.84M 3s
233000K .......... .......... .......... .......... .......... 87% 7.72M 3s
233050K .......... .......... .......... .......... .......... 87% 10.4M 3s
233100K .......... .......... .......... .......... .......... 87% 6.98M 3s
233150K .......... .......... .......... .......... .......... 87% 7.11M 3s
233200K .......... .......... .......... .......... .......... 87% 11.5M 3s
233250K .......... .......... .......... .......... .......... 87% 8.42M 3s
233300K .......... .......... .......... .......... .......... 87% 3.82M 3s
233350K .......... .......... .......... .......... .......... 87% 75.9M 3s
233400K .......... .......... .......... .......... .......... 87% 6.22M 3s
233450K .......... .......... .......... .......... .......... 87% 241M 3s
233500K .......... .......... .......... .......... .......... 87% 8.18M 3s
233550K .......... .......... .......... .......... .......... 87% 13.6M 3s
233600K .......... .......... .......... .......... .......... 88% 6.22M 3s
233650K .......... .......... .......... .......... .......... 88% 6.86M 3s
233700K .......... .......... .......... .......... .......... 88% 6.75M 3s
233750K .......... .......... .......... .......... .......... 88% 6.79M 3s
233800K .......... .......... .......... .......... .......... 88% 8.69M 3s
233850K .......... .......... .......... .......... .......... 88% 8.74M 3s
233900K .......... .......... .......... .......... .......... 88% 9.41M 3s
233950K .......... .......... .......... .......... .......... 88% 7.97M 3s
234000K .......... .......... .......... .......... .......... 88% 8.70M 3s
234050K .......... .......... .......... .......... .......... 88% 8.38M 3s
234100K .......... .......... .......... .......... .......... 88% 7.56M 3s
234150K .......... .......... .......... .......... .......... 88% 11.1M 3s
234200K .......... .......... .......... .......... .......... 88% 6.65M 3s
234250K .......... .......... .......... .......... .......... 88% 10.9M 3s
234300K .......... .......... .......... .......... .......... 88% 11.7M 3s
234350K .......... .......... .......... .......... .......... 88% 10.3M 3s
234400K .......... .......... .......... .......... .......... 88% 8.33M 3s
234450K .......... .......... .......... .......... .......... 88% 8.12M 3s
234500K .......... .......... .......... .......... .......... 88% 13.1M 3s
234550K .......... .......... .......... .......... .......... 88% 4.94M 3s
234600K .......... .......... .......... .......... .......... 88% 72.0M 3s
234650K .......... .......... .......... .......... .......... 88% 10.2M 3s
234700K .......... .......... .......... .......... .......... 88% 8.00M 3s
234750K .......... .......... .......... .......... .......... 88% 9.99M 3s
234800K .......... .......... .......... .......... .......... 88% 10.4M 3s
234850K .......... .......... .......... .......... .......... 88% 7.32M 3s
234900K .......... .......... .......... .......... .......... 88% 14.6M 3s
234950K .......... .......... .......... .......... .......... 88% 7.54M 3s
235000K .......... .......... .......... .......... .......... 88% 11.3M 3s
235050K .......... .......... .......... .......... .......... 88% 14.2M 3s
235100K .......... .......... .......... .......... .......... 88% 9.48M 3s
235150K .......... .......... .......... .......... .......... 88% 8.54M 3s
235200K .......... .......... .......... .......... .......... 88% 8.61M 3s
235250K .......... .......... .......... .......... .......... 88% 7.83M 3s
235300K .......... .......... .......... .......... .......... 88% 12.4M 3s
235350K .......... .......... .......... .......... .......... 88% 10.1M 3s
235400K .......... .......... .......... .......... .......... 88% 11.6M 3s
235450K .......... .......... .......... .......... .......... 88% 7.41M 3s
235500K .......... .......... .......... .......... .......... 88% 5.55M 3s
235550K .......... .......... .......... .......... .......... 88% 61.8M 3s
235600K .......... .......... .......... .......... .......... 88% 7.41M 3s
235650K .......... .......... .......... .......... .......... 88% 8.94M 3s
235700K .......... .......... .......... .......... .......... 88% 6.45M 3s
235750K .......... .......... .......... .......... .......... 88% 11.8M 3s
235800K .......... .......... .......... .......... .......... 88% 8.91M 3s
235850K .......... .......... .......... .......... .......... 88% 6.53M 3s
235900K .......... .......... .......... .......... .......... 88% 9.18M 2s
235950K .......... .......... .......... .......... .......... 88% 10.4M 2s
236000K .......... .......... .......... .......... .......... 88% 8.58M 2s
236050K .......... .......... .......... .......... .......... 88% 3.99M 2s
236100K .......... .......... .......... .......... .......... 88% 16.4M 2s
236150K .......... .......... .......... .......... .......... 88% 14.5M 2s
236200K .......... .......... .......... .......... .......... 88% 6.61M 2s
236250K .......... .......... .......... .......... .......... 88% 6.14M 2s
236300K .......... .......... .......... .......... .......... 89% 6.12M 2s
236350K .......... .......... .......... .......... .......... 89% 6.17M 2s
236400K .......... .......... .......... .......... .......... 89% 7.94M 2s
236450K .......... .......... .......... .......... .......... 89% 7.19M 2s
236500K .......... .......... .......... .......... .......... 89% 7.45M 2s
236550K .......... .......... .......... .......... .......... 89% 8.84M 2s
236600K .......... .......... .......... .......... .......... 89% 6.47M 2s
236650K .......... .......... .......... .......... .......... 89% 13.3M 2s
236700K .......... .......... .......... .......... .......... 89% 6.27M 2s
236750K .......... .......... .......... .......... .......... 89% 12.0M 2s
236800K .......... .......... .......... .......... .......... 89% 12.8M 2s
236850K .......... .......... .......... .......... .......... 89% 6.61M 2s
236900K .......... .......... .......... .......... .......... 89% 11.2M 2s
236950K .......... .......... .......... .......... .......... 89% 8.03M 2s
237000K .......... .......... .......... .......... .......... 89% 8.79M 2s
237050K .......... .......... .......... .......... .......... 89% 11.7M 2s
237100K .......... .......... .......... .......... .......... 89% 8.34M 2s
237150K .......... .......... .......... .......... .......... 89% 8.94M 2s
237200K .......... .......... .......... .......... .......... 89% 11.2M 2s
237250K .......... .......... .......... .......... .......... 89% 11.3M 2s
237300K .......... .......... .......... .......... .......... 89% 12.2M 2s
237350K .......... .......... .......... .......... .......... 89% 12.9M 2s
237400K .......... .......... .......... .......... .......... 89% 12.5M 2s
237450K .......... .......... .......... .......... .......... 89% 6.91M 2s
237500K .......... .......... .......... .......... .......... 89% 28.0M 2s
237550K .......... .......... .......... .......... .......... 89% 24.6M 2s
237600K .......... .......... .......... .......... .......... 89% 11.8M 2s
237650K .......... .......... .......... .......... .......... 89% 13.6M 2s
237700K .......... .......... .......... .......... .......... 89% 10.2M 2s
237750K .......... .......... .......... .......... .......... 89% 13.3M 2s
237800K .......... .......... .......... .......... .......... 89% 27.1M 2s
237850K .......... .......... .......... .......... .......... 89% 8.39M 2s
237900K .......... .......... .......... .......... .......... 89% 31.1M 2s
237950K .......... .......... .......... .......... .......... 89% 8.63M 2s
238000K .......... .......... .......... .......... .......... 89% 12.7M 2s
238050K .......... .......... .......... .......... .......... 89% 19.2M 2s
238100K .......... .......... .......... .......... .......... 89% 9.67M 2s
238150K .......... .......... .......... .......... .......... 89% 12.5M 2s
238200K .......... .......... .......... .......... .......... 89% 12.2M 2s
238250K .......... .......... .......... .......... .......... 89% 12.2M 2s
238300K .......... .......... .......... .......... .......... 89% 14.0M 2s
238350K .......... .......... .......... .......... .......... 89% 18.4M 2s
238400K .......... .......... .......... .......... .......... 89% 22.2M 2s
238450K .......... .......... .......... .......... .......... 89% 9.97M 2s
238500K .......... .......... .......... .......... .......... 89% 17.2M 2s
238550K .......... .......... .......... .......... .......... 89% 11.1M 2s
238600K .......... .......... .......... .......... .......... 89% 11.6M 2s
238650K .......... .......... .......... .......... .......... 89% 21.3M 2s
238700K .......... .......... .......... .......... .......... 89% 12.2M 2s
238750K .......... .......... .......... .......... .......... 89% 19.0M 2s
238800K .......... .......... .......... .......... .......... 89% 13.9M 2s
238850K .......... .......... .......... .......... .......... 89% 18.8M 2s
238900K .......... .......... .......... .......... .......... 89% 15.9M 2s
238950K .......... .......... .......... .......... .......... 90% 15.9M 2s
239000K .......... .......... .......... .......... .......... 90% 12.9M 2s
239050K .......... .......... .......... .......... .......... 90% 11.9M 2s
239100K .......... .......... .......... .......... .......... 90% 15.3M 2s
239150K .......... .......... .......... .......... .......... 90% 52.1M 2s
239200K .......... .......... .......... .......... .......... 90% 13.1M 2s
239250K .......... .......... .......... .......... .......... 90% 12.1M 2s
239300K .......... .......... .......... .......... .......... 90% 207M 2s
239350K .......... .......... .......... .......... .......... 90% 12.3M 2s
239400K .......... .......... .......... .......... .......... 90% 12.9M 2s
239450K .......... .......... .......... .......... .......... 90% 15.8M 2s
239500K .......... .......... .......... .......... .......... 90% 36.4M 2s
239550K .......... .......... .......... .......... .......... 90% 12.7M 2s
239600K .......... .......... .......... .......... .......... 90% 14.9M 2s
239650K .......... .......... .......... .......... .......... 90% 52.2M 2s
239700K .......... .......... .......... .......... .......... 90% 11.9M 2s
239750K .......... .......... .......... .......... .......... 90% 5.32M 2s
239800K .......... .......... .......... .......... .......... 90% 56.1M 2s
239850K .......... .......... .......... .......... .......... 90% 21.3M 2s
239900K .......... .......... .......... .......... .......... 90% 14.5M 2s
239950K .......... .......... .......... .......... .......... 90% 12.2M 2s
240000K .......... .......... .......... .......... .......... 90% 12.5M 2s
240050K .......... .......... .......... .......... .......... 90% 12.9M 2s
240100K .......... .......... .......... .......... .......... 90% 11.9M 2s
240150K .......... .......... .......... .......... .......... 90% 12.7M 2s
240200K .......... .......... .......... .......... .......... 90% 10.8M 2s
240250K .......... .......... .......... .......... .......... 90% 12.1M 2s
240300K .......... .......... .......... .......... .......... 90% 12.8M 2s
240350K .......... .......... .......... .......... .......... 90% 10.5M 2s
240400K .......... .......... .......... .......... .......... 90% 15.2M 2s
240450K .......... .......... .......... .......... .......... 90% 12.1M 2s
240500K .......... .......... .......... .......... .......... 90% 12.5M 2s
240550K .......... .......... .......... .......... .......... 90% 14.0M 2s
240600K .......... .......... .......... .......... .......... 90% 9.74M 2s
240650K .......... .......... .......... .......... .......... 90% 12.0M 2s
240700K .......... .......... .......... .......... .......... 90% 11.3M 2s
240750K .......... .......... .......... .......... .......... 90% 12.5M 2s
240800K .......... .......... .......... .......... .......... 90% 12.4M 2s
240850K .......... .......... .......... .......... .......... 90% 11.7M 2s
240900K .......... .......... .......... .......... .......... 90% 12.7M 2s
240950K .......... .......... .......... .......... .......... 90% 13.4M 2s
241000K .......... .......... .......... .......... .......... 90% 15.5M 2s
241050K .......... .......... .......... .......... .......... 90% 21.9M 2s
241100K .......... .......... .......... .......... .......... 90% 8.51M 2s
241150K .......... .......... .......... .......... .......... 90% 20.7M 2s
241200K .......... .......... .......... .......... .......... 90% 11.4M 2s
241250K .......... .......... .......... .......... .......... 90% 11.2M 2s
241300K .......... .......... .......... .......... .......... 90% 31.6M 2s
241350K .......... .......... .......... .......... .......... 90% 13.4M 2s
241400K .......... .......... .......... .......... .......... 90% 11.0M 2s
241450K .......... .......... .......... .......... .......... 90% 10.5M 2s
241500K .......... .......... .......... .......... .......... 90% 13.8M 2s
241550K .......... .......... .......... .......... .......... 90% 28.9M 2s
241600K .......... .......... .......... .......... .......... 91% 10.9M 2s
241650K .......... .......... .......... .......... .......... 91% 13.4M 2s
241700K .......... .......... .......... .......... .......... 91% 11.7M 2s
241750K .......... .......... .......... .......... .......... 91% 30.9M 2s
241800K .......... .......... .......... .......... .......... 91% 16.0M 2s
241850K .......... .......... .......... .......... .......... 91% 10.9M 2s
241900K .......... .......... .......... .......... .......... 91% 50.4M 2s
241950K .......... .......... .......... .......... .......... 91% 12.1M 2s
242000K .......... .......... .......... .......... .......... 91% 19.6M 2s
242050K .......... .......... .......... .......... .......... 91% 11.4M 2s
242100K .......... .......... .......... .......... .......... 91% 23.8M 2s
242150K .......... .......... .......... .......... .......... 91% 11.2M 2s
242200K .......... .......... .......... .......... .......... 91% 20.6M 2s
242250K .......... .......... .......... .......... .......... 91% 19.5M 2s
242300K .......... .......... .......... .......... .......... 91% 12.4M 2s
242350K .......... .......... .......... .......... .......... 91% 11.8M 2s
242400K .......... .......... .......... .......... .......... 91% 24.0M 2s
242450K .......... .......... .......... .......... .......... 91% 16.5M 2s
242500K .......... .......... .......... .......... .......... 91% 11.9M 2s
242550K .......... .......... .......... .......... .......... 91% 16.9M 2s
242600K .......... .......... .......... .......... .......... 91% 13.4M 2s
242650K .......... .......... .......... .......... .......... 91% 18.7M 2s
242700K .......... .......... .......... .......... .......... 91% 12.0M 2s
242750K .......... .......... .......... .......... .......... 91% 12.5M 2s
242800K .......... .......... .......... .......... .......... 91% 13.6M 2s
242850K .......... .......... .......... .......... .......... 91% 7.29M 2s
242900K .......... .......... .......... .......... .......... 91% 68.8M 2s
242950K .......... .......... .......... .......... .......... 91% 36.0M 2s
243000K .......... .......... .......... .......... .......... 91% 11.4M 2s
243050K .......... .......... .......... .......... .......... 91% 8.35M 2s
243100K .......... .......... .......... .......... .......... 91% 20.6M 2s
243150K .......... .......... .......... .......... .......... 91% 11.5M 2s
243200K .......... .......... .......... .......... .......... 91% 8.71M 2s
243250K .......... .......... .......... .......... .......... 91% 25.7M 2s
243300K .......... .......... .......... .......... .......... 91% 12.3M 2s
243350K .......... .......... .......... .......... .......... 91% 11.5M 2s
243400K .......... .......... .......... .......... .......... 91% 10.8M 2s
243450K .......... .......... .......... .......... .......... 91% 15.6M 2s
243500K .......... .......... .......... .......... .......... 91% 12.6M 2s
243550K .......... .......... .......... .......... .......... 91% 11.6M 2s
243600K .......... .......... .......... .......... .......... 91% 10.5M 2s
243650K .......... .......... .......... .......... .......... 91% 8.72M 2s
243700K .......... .......... .......... .......... .......... 91% 45.3M 2s
243750K .......... .......... .......... .......... .......... 91% 16.1M 2s
243800K .......... .......... .......... .......... .......... 91% 13.0M 2s
243850K .......... .......... .......... .......... .......... 91% 8.33M 2s
243900K .......... .......... .......... .......... .......... 91% 9.40M 2s
243950K .......... .......... .......... .......... .......... 91% 9.81M 2s
244000K .......... .......... .......... .......... .......... 91% 15.2M 2s
244050K .......... .......... .......... .......... .......... 91% 13.1M 2s
244100K .......... .......... .......... .......... .......... 91% 11.2M 2s
244150K .......... .......... .......... .......... .......... 91% 10.7M 2s
244200K .......... .......... .......... .......... .......... 91% 10.1M 2s
244250K .......... .......... .......... .......... .......... 92% 11.3M 2s
244300K .......... .......... .......... .......... .......... 92% 11.1M 2s
244350K .......... .......... .......... .......... .......... 92% 12.2M 2s
244400K .......... .......... .......... .......... .......... 92% 12.9M 2s
244450K .......... .......... .......... .......... .......... 92% 11.7M 2s
244500K .......... .......... .......... .......... .......... 92% 12.0M 2s
244550K .......... .......... .......... .......... .......... 92% 12.2M 2s
244600K .......... .......... .......... .......... .......... 92% 12.0M 2s
244650K .......... .......... .......... .......... .......... 92% 12.2M 2s
244700K .......... .......... .......... .......... .......... 92% 11.5M 2s
244750K .......... .......... .......... .......... .......... 92% 11.8M 2s
244800K .......... .......... .......... .......... .......... 92% 31.3M 2s
244850K .......... .......... .......... .......... .......... 92% 12.2M 2s
244900K .......... .......... .......... .......... .......... 92% 13.4M 2s
244950K .......... .......... .......... .......... .......... 92% 8.97M 2s
245000K .......... .......... .......... .......... .......... 92% 20.1M 2s
245050K .......... .......... .......... .......... .......... 92% 15.2M 2s
245100K .......... .......... .......... .......... .......... 92% 10.7M 2s
245150K .......... .......... .......... .......... .......... 92% 18.5M 2s
245200K .......... .......... .......... .......... .......... 92% 36.1M 2s
245250K .......... .......... .......... .......... .......... 92% 13.9M 2s
245300K .......... .......... .......... .......... .......... 92% 15.0M 2s
245350K .......... .......... .......... .......... .......... 92% 13.5M 2s
245400K .......... .......... .......... .......... .......... 92% 33.1M 2s
245450K .......... .......... .......... .......... .......... 92% 21.4M 2s
245500K .......... .......... .......... .......... .......... 92% 11.2M 2s
245550K .......... .......... .......... .......... .......... 92% 17.7M 2s
245600K .......... .......... .......... .......... .......... 92% 13.2M 2s
245650K .......... .......... .......... .......... .......... 92% 33.8M 2s
245700K .......... .......... .......... .......... .......... 92% 14.3M 2s
245750K .......... .......... .......... .......... .......... 92% 16.6M 2s
245800K .......... .......... .......... .......... .......... 92% 13.4M 2s
245850K .......... .......... .......... .......... .......... 92% 6.60M 2s
245900K .......... .......... .......... .......... .......... 92% 62.8M 2s
245950K .......... .......... .......... .......... .......... 92% 71.0M 2s
246000K .......... .......... .......... .......... .......... 92% 16.1M 2s
246050K .......... .......... .......... .......... .......... 92% 14.5M 2s
246100K .......... .......... .......... .......... .......... 92% 12.7M 2s
246150K .......... .......... .......... .......... .......... 92% 16.2M 2s
246200K .......... .......... .......... .......... .......... 92% 12.4M 2s
246250K .......... .......... .......... .......... .......... 92% 13.9M 2s
246300K .......... .......... .......... .......... .......... 92% 14.3M 2s
246350K .......... .......... .......... .......... .......... 92% 15.3M 2s
246400K .......... .......... .......... .......... .......... 92% 13.2M 2s
246450K .......... .......... .......... .......... .......... 92% 11.8M 2s
246500K .......... .......... .......... .......... .......... 92% 44.4M 2s
246550K .......... .......... .......... .......... .......... 92% 20.8M 2s
246600K .......... .......... .......... .......... .......... 92% 17.3M 2s
246650K .......... .......... .......... .......... .......... 92% 19.2M 2s
246700K .......... .......... .......... .......... .......... 92% 22.4M 2s
246750K .......... .......... .......... .......... .......... 92% 46.4M 2s
246800K .......... .......... .......... .......... .......... 92% 18.6M 2s
246850K .......... .......... .......... .......... .......... 92% 16.8M 2s
246900K .......... .......... .......... .......... .......... 93% 16.9M 2s
246950K .......... .......... .......... .......... .......... 93% 20.0M 2s
247000K .......... .......... .......... .......... .......... 93% 27.7M 2s
247050K .......... .......... .......... .......... .......... 93% 39.8M 2s
247100K .......... .......... .......... .......... .......... 93% 18.1M 2s
247150K .......... .......... .......... .......... .......... 93% 21.1M 2s
247200K .......... .......... .......... .......... .......... 93% 9.67M 2s
247250K .......... .......... .......... .......... .......... 93% 34.5M 2s
247300K .......... .......... .......... .......... .......... 93% 15.8M 2s
247350K .......... .......... .......... .......... .......... 93% 18.2M 2s
247400K .......... .......... .......... .......... .......... 93% 17.5M 2s
247450K .......... .......... .......... .......... .......... 93% 12.4M 2s
247500K .......... .......... .......... .......... .......... 93% 18.4M 2s
247550K .......... .......... .......... .......... .......... 93% 15.1M 2s
247600K .......... .......... .......... .......... .......... 93% 16.2M 2s
247650K .......... .......... .......... .......... .......... 93% 20.3M 1s
247700K .......... .......... .......... .......... .......... 93% 14.5M 1s
247750K .......... .......... .......... .......... .......... 93% 15.8M 1s
247800K .......... .......... .......... .......... .......... 93% 19.4M 1s
247850K .......... .......... .......... .......... .......... 93% 18.0M 1s
247900K .......... .......... .......... .......... .......... 93% 22.7M 1s
247950K .......... .......... .......... .......... .......... 93% 11.7M 1s
248000K .......... .......... .......... .......... .......... 93% 49.0M 1s
248050K .......... .......... .......... .......... .......... 93% 16.5M 1s
248100K .......... .......... .......... .......... .......... 93% 15.4M 1s
248150K .......... .......... .......... .......... .......... 93% 18.3M 1s
248200K .......... .......... .......... .......... .......... 93% 18.0M 1s
248250K .......... .......... .......... .......... .......... 93% 17.9M 1s
248300K .......... .......... .......... .......... .......... 93% 18.5M 1s
248350K .......... .......... .......... .......... .......... 93% 15.4M 1s
248400K .......... .......... .......... .......... .......... 93% 20.8M 1s
248450K .......... .......... .......... .......... .......... 93% 14.4M 1s
248500K .......... .......... .......... .......... .......... 93% 20.0M 1s
248550K .......... .......... .......... .......... .......... 93% 14.6M 1s
248600K .......... .......... .......... .......... .......... 93% 16.1M 1s
248650K .......... .......... .......... .......... .......... 93% 16.7M 1s
248700K .......... .......... .......... .......... .......... 93% 17.3M 1s
248750K .......... .......... .......... .......... .......... 93% 17.3M 1s
248800K .......... .......... .......... .......... .......... 93% 22.4M 1s
248850K .......... .......... .......... .......... .......... 93% 11.5M 1s
248900K .......... .......... .......... .......... .......... 93% 56.2M 1s
248950K .......... .......... .......... .......... .......... 93% 12.9M 1s
249000K .......... .......... .......... .......... .......... 93% 20.1M 1s
249050K .......... .......... .......... .......... .......... 93% 15.2M 1s
249100K .......... .......... .......... .......... .......... 93% 12.6M 1s
249150K .......... .......... .......... .......... .......... 93% 19.9M 1s
249200K .......... .......... .......... .......... .......... 93% 12.6M 1s
249250K .......... .......... .......... .......... .......... 93% 16.7M 1s
249300K .......... .......... .......... .......... .......... 93% 49.6M 1s
249350K .......... .......... .......... .......... .......... 93% 6.27M 1s
249400K .......... .......... .......... .......... .......... 93% 58.4M 1s
249450K .......... .......... .......... .......... .......... 93% 33.2M 1s
249500K .......... .......... .......... .......... .......... 93% 13.9M 1s
249550K .......... .......... .......... .......... .......... 94% 15.5M 1s
249600K .......... .......... .......... .......... .......... 94% 9.70M 1s
249650K .......... .......... .......... .......... .......... 94% 12.5M 1s
249700K .......... .......... .......... .......... .......... 94% 10.3M 1s
249750K .......... .......... .......... .......... .......... 94% 11.2M 1s
249800K .......... .......... .......... .......... .......... 94% 12.1M 1s
249850K .......... .......... .......... .......... .......... 94% 13.0M 1s
249900K .......... .......... .......... .......... .......... 94% 13.1M 1s
249950K .......... .......... .......... .......... .......... 94% 13.4M 1s
250000K .......... .......... .......... .......... .......... 94% 12.3M 1s
250050K .......... .......... .......... .......... .......... 94% 11.8M 1s
250100K .......... .......... .......... .......... .......... 94% 9.78M 1s
250150K .......... .......... .......... .......... .......... 94% 11.4M 1s
250200K .......... .......... .......... .......... .......... 94% 11.9M 1s
250250K .......... .......... .......... .......... .......... 94% 13.5M 1s
250300K .......... .......... .......... .......... .......... 94% 20.6M 1s
250350K .......... .......... .......... .......... .......... 94% 8.68M 1s
250400K .......... .......... .......... .......... .......... 94% 21.6M 1s
250450K .......... .......... .......... .......... .......... 94% 9.91M 1s
250500K .......... .......... .......... .......... .......... 94% 12.4M 1s
250550K .......... .......... .......... .......... .......... 94% 55.8M 1s
250600K .......... .......... .......... .......... .......... 94% 8.17M 1s
250650K .......... .......... .......... .......... .......... 94% 13.4M 1s
250700K .......... .......... .......... .......... .......... 94% 9.51M 1s
250750K .......... .......... .......... .......... .......... 94% 12.0M 1s
250800K .......... .......... .......... .......... .......... 94% 17.9M 1s
250850K .......... .......... .......... .......... .......... 94% 8.53M 1s
250900K .......... .......... .......... .......... .......... 94% 5.97M 1s
250950K .......... .......... .......... .......... .......... 94% 43.4M 1s
251000K .......... .......... .......... .......... .......... 94% 53.6M 1s
251050K .......... .......... .......... .......... .......... 94% 7.31M 1s
251100K .......... .......... .......... .......... .......... 94% 12.9M 1s
251150K .......... .......... .......... .......... .......... 94% 11.0M 1s
251200K .......... .......... .......... .......... .......... 94% 11.9M 1s
251250K .......... .......... .......... .......... .......... 94% 11.3M 1s
251300K .......... .......... .......... .......... .......... 94% 12.9M 1s
251350K .......... .......... .......... .......... .......... 94% 10.7M 1s
251400K .......... .......... .......... .......... .......... 94% 13.1M 1s
251450K .......... .......... .......... .......... .......... 94% 11.0M 1s
251500K .......... .......... .......... .......... .......... 94% 13.4M 1s
251550K .......... .......... .......... .......... .......... 94% 11.2M 1s
251600K .......... .......... .......... .......... .......... 94% 14.6M 1s
251650K .......... .......... .......... .......... .......... 94% 12.7M 1s
251700K .......... .......... .......... .......... .......... 94% 13.9M 1s
251750K .......... .......... .......... .......... .......... 94% 12.7M 1s
251800K .......... .......... .......... .......... .......... 94% 14.9M 1s
251850K .......... .......... .......... .......... .......... 94% 11.5M 1s
251900K .......... .......... .......... .......... .......... 94% 13.4M 1s
251950K .......... .......... .......... .......... .......... 94% 13.2M 1s
252000K .......... .......... .......... .......... .......... 94% 13.0M 1s
252050K .......... .......... .......... .......... .......... 94% 43.3M 1s
252100K .......... .......... .......... .......... .......... 94% 12.4M 1s
252150K .......... .......... .......... .......... .......... 94% 12.9M 1s
252200K .......... .......... .......... .......... .......... 95% 12.3M 1s
252250K .......... .......... .......... .......... .......... 95% 12.1M 1s
252300K .......... .......... .......... .......... .......... 95% 12.7M 1s
252350K .......... .......... .......... .......... .......... 95% 12.6M 1s
252400K .......... .......... .......... .......... .......... 95% 21.5M 1s
252450K .......... .......... .......... .......... .......... 95% 8.61M 1s
252500K .......... .......... .......... .......... .......... 95% 20.4M 1s
252550K .......... .......... .......... .......... .......... 95% 13.1M 1s
252600K .......... .......... .......... .......... .......... 95% 28.6M 1s
252650K .......... .......... .......... .......... .......... 95% 9.88M 1s
252700K .......... .......... .......... .......... .......... 95% 17.2M 1s
252750K .......... .......... .......... .......... .......... 95% 14.0M 1s
252800K .......... .......... .......... .......... .......... 95% 22.0M 1s
252850K .......... .......... .......... .......... .......... 95% 22.2M 1s
252900K .......... .......... .......... .......... .......... 95% 12.9M 1s
252950K .......... .......... .......... .......... .......... 95% 17.1M 1s
253000K .......... .......... .......... .......... .......... 95% 14.0M 1s
253050K .......... .......... .......... .......... .......... 95% 16.4M 1s
253100K .......... .......... .......... .......... .......... 95% 40.9M 1s
253150K .......... .......... .......... .......... .......... 95% 13.6M 1s
253200K .......... .......... .......... .......... .......... 95% 14.1M 1s
253250K .......... .......... .......... .......... .......... 95% 16.3M 1s
253300K .......... .......... .......... .......... .......... 95% 44.3M 1s
253350K .......... .......... .......... .......... .......... 95% 12.9M 1s
253400K .......... .......... .......... .......... .......... 95% 13.6M 1s
253450K .......... .......... .......... .......... .......... 95% 58.2M 1s
253500K .......... .......... .......... .......... .......... 95% 13.2M 1s
253550K .......... .......... .......... .......... .......... 95% 12.3M 1s
253600K .......... .......... .......... .......... .......... 95% 88.6M 1s
253650K .......... .......... .......... .......... .......... 95% 12.5M 1s
253700K .......... .......... .......... .......... .......... 95% 5.69M 1s
253750K .......... .......... .......... .......... .......... 95% 166M 1s
253800K .......... .......... .......... .......... .......... 95% 15.6M 1s
253850K .......... .......... .......... .......... .......... 95% 14.6M 1s
253900K .......... .......... .......... .......... .......... 95% 46.9M 1s
253950K .......... .......... .......... .......... .......... 95% 9.71M 1s
254000K .......... .......... .......... .......... .......... 95% 12.2M 1s
254050K .......... .......... .......... .......... .......... 95% 17.8M 1s
254100K .......... .......... .......... .......... .......... 95% 12.4M 1s
254150K .......... .......... .......... .......... .......... 95% 11.6M 1s
254200K .......... .......... .......... .......... .......... 95% 8.73M 1s
254250K .......... .......... .......... .......... .......... 95% 18.7M 1s
254300K .......... .......... .......... .......... .......... 95% 12.5M 1s
254350K .......... .......... .......... .......... .......... 95% 8.69M 1s
254400K .......... .......... .......... .......... .......... 95% 43.8M 1s
254450K .......... .......... .......... .......... .......... 95% 14.9M 1s
254500K .......... .......... .......... .......... .......... 95% 12.1M 1s
254550K .......... .......... .......... .......... .......... 95% 15.8M 1s
254600K .......... .......... .......... .......... .......... 95% 13.2M 1s
254650K .......... .......... .......... .......... .......... 95% 18.3M 1s
254700K .......... .......... .......... .......... .......... 95% 10.0M 1s
254750K .......... .......... .......... .......... .......... 95% 14.2M 1s
254800K .......... .......... .......... .......... .......... 95% 43.6M 1s
254850K .......... .......... .......... .......... .......... 96% 12.1M 1s
254900K .......... .......... .......... .......... .......... 96% 12.9M 1s
254950K .......... .......... .......... .......... .......... 96% 11.9M 1s
255000K .......... .......... .......... .......... .......... 96% 16.3M 1s
255050K .......... .......... .......... .......... .......... 96% 37.7M 1s
255100K .......... .......... .......... .......... .......... 96% 12.0M 1s
255150K .......... .......... .......... .......... .......... 96% 12.6M 1s
255200K .......... .......... .......... .......... .......... 96% 11.4M 1s
255250K .......... .......... .......... .......... .......... 96% 20.5M 1s
255300K .......... .......... .......... .......... .......... 96% 37.3M 1s
255350K .......... .......... .......... .......... .......... 96% 11.8M 1s
255400K .......... .......... .......... .......... .......... 96% 14.3M 1s
255450K .......... .......... .......... .......... .......... 96% 17.7M 1s
255500K .......... .......... .......... .......... .......... 96% 27.4M 1s
255550K .......... .......... .......... .......... .......... 96% 12.8M 1s
255600K .......... .......... .......... .......... .......... 96% 15.0M 1s
255650K .......... .......... .......... .......... .......... 96% 40.5M 1s
255700K .......... .......... .......... .......... .......... 96% 11.7M 1s
255750K .......... .......... .......... .......... .......... 96% 12.8M 1s
255800K .......... .......... .......... .......... .......... 96% 19.7M 1s
255850K .......... .......... .......... .......... .......... 96% 28.1M 1s
255900K .......... .......... .......... .......... .......... 96% 6.62M 1s
255950K .......... .......... .......... .......... .......... 96% 98.1M 1s
256000K .......... .......... .......... .......... .......... 96% 14.9M 1s
256050K .......... .......... .......... .......... .......... 96% 13.5M 1s
256100K .......... .......... .......... .......... .......... 96% 12.2M 1s
256150K .......... .......... .......... .......... .......... 96% 14.3M 1s
256200K .......... .......... .......... .......... .......... 96% 11.1M 1s
256250K .......... .......... .......... .......... .......... 96% 20.0M 1s
256300K .......... .......... .......... .......... .......... 96% 12.5M 1s
256350K .......... .......... .......... .......... .......... 96% 16.4M 1s
256400K .......... .......... .......... .......... .......... 96% 17.1M 1s
256450K .......... .......... .......... .......... .......... 96% 11.2M 1s
256500K .......... .......... .......... .......... .......... 96% 23.0M 1s
256550K .......... .......... .......... .......... .......... 96% 16.9M 1s
256600K .......... .......... .......... .......... .......... 96% 12.4M 1s
256650K .......... .......... .......... .......... .......... 96% 16.7M 1s
256700K .......... .......... .......... .......... .......... 96% 16.8M 1s
256750K .......... .......... .......... .......... .......... 96% 44.5M 1s
256800K .......... .......... .......... .......... .......... 96% 18.0M 1s
256850K .......... .......... .......... .......... .......... 96% 13.5M 1s
256900K .......... .......... .......... .......... .......... 96% 33.0M 1s
256950K .......... .......... .......... .......... .......... 96% 15.8M 1s
257000K .......... .......... .......... .......... .......... 96% 35.4M 1s
257050K .......... .......... .......... .......... .......... 96% 9.14M 1s
257100K .......... .......... .......... .......... .......... 96% 37.4M 1s
257150K .......... .......... .......... .......... .......... 96% 61.8M 1s
257200K .......... .......... .......... .......... .......... 96% 13.2M 1s
257250K .......... .......... .......... .......... .......... 96% 18.5M 1s
257300K .......... .......... .......... .......... .......... 96% 14.1M 1s
257350K .......... .......... .......... .......... .......... 96% 25.8M 1s
257400K .......... .......... .......... .......... .......... 96% 12.0M 1s
257450K .......... .......... .......... .......... .......... 96% 22.1M 1s
257500K .......... .......... .......... .......... .......... 97% 12.7M 1s
257550K .......... .......... .......... .......... .......... 97% 14.9M 1s
257600K .......... .......... .......... .......... .......... 97% 11.1M 1s
257650K .......... .......... .......... .......... .......... 97% 17.6M 1s
257700K .......... .......... .......... .......... .......... 97% 11.3M 1s
257750K .......... .......... .......... .......... .......... 97% 22.4M 1s
257800K .......... .......... .......... .......... .......... 97% 16.2M 1s
257850K .......... .......... .......... .......... .......... 97% 10.4M 1s
257900K .......... .......... .......... .......... .......... 97% 16.7M 1s
257950K .......... .......... .......... .......... .......... 97% 17.8M 1s
258000K .......... .......... .......... .......... .......... 97% 7.00M 1s
258050K .......... .......... .......... .......... .......... 97% 109M 1s
258100K .......... .......... .......... .......... .......... 97% 12.6M 1s
258150K .......... .......... .......... .......... .......... 97% 16.6M 1s
258200K .......... .......... .......... .......... .......... 97% 9.77M 1s
258250K .......... .......... .......... .......... .......... 97% 16.5M 1s
258300K .......... .......... .......... .......... .......... 97% 19.8M 1s
258350K .......... .......... .......... .......... .......... 97% 7.56M 1s
258400K .......... .......... .......... .......... .......... 97% 17.7M 1s
258450K .......... .......... .......... .......... .......... 97% 9.52M 1s
258500K .......... .......... .......... .......... .......... 97% 13.7M 1s
258550K .......... .......... .......... .......... .......... 97% 5.57M 1s
258600K .......... .......... .......... .......... .......... 97% 83.9M 1s
258650K .......... .......... .......... .......... .......... 97% 25.0M 1s
258700K .......... .......... .......... .......... .......... 97% 8.36M 1s
258750K .......... .......... .......... .......... .......... 97% 14.8M 1s
258800K .......... .......... .......... .......... .......... 97% 8.63M 1s
258850K .......... .......... .......... .......... .......... 97% 10.7M 1s
258900K .......... .......... .......... .......... .......... 97% 5.18M 1s
258950K .......... .......... .......... .......... .......... 97% 74.2M 1s
259000K .......... .......... .......... .......... .......... 97% 14.3M 1s
259050K .......... .......... .......... .......... .......... 97% 5.48M 1s
259100K .......... .......... .......... .......... .......... 97% 85.1M 1s
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265500K .......... 100% 67.3M=22s
2024-07-26 09:47:48 (11.8 MB/s) - ‘ESPbeta.tgz’ saved [271882371/271882371]
+ tar -xf ESPbeta.tgz
+ rm -rf EngSketchPad/data/Slugs
+ python --version
Python 3.11.9
+ [[ '' == *\.\i\f\o\r\t ]]
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.7.0 with contents:
bin
include
lib
share
Info: Python exec /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 = /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
EFCOMP = gfortran
CARCH = LINUX64
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.7.0
CASARCH = .
CASREV = 7.7
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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.7.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.7
++ CASREV=7.7
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/bin:/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/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:/usr/local/bin:/usr/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=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ '[' -z /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.7.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include 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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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=7.7 -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.7.0 -I../include -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
BOOST_AUTO_TEST_CASE( multiply_deriv2 )
^
../util/SurrealS4_btest.cpp:19:42: note: in definition of macro ‘BOOST_AUTO_TEST_CASE’
#define BOOST_AUTO_TEST_CASE( fun ) void fun()
^
./SurrealS4
SurrealS4_test_suite Complete!
make -C ../util
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a ./egadsUVmap.o uvmap_cpu_message.o uvmap_ibfibf.o uvmap_message.o uvmap_version.o uvmap_gen_uv.o uvmap_inl_uv_bnd.o EG_uvmap_Read.o uvmap_chk_edge_ratio.o uvmap_idibe.o uvmap_write.o uvmap_ibeibe.o uvmap_chk_area_uv.o uvmap_gen.o uvmap_malloc.o uvmap_to_egads.o EG_uvmap_Write.o uvmap_iccibe.o EG_uvmapGen.o EG_uvmapTest.o uvmap_read.o uvmap_ibfin.o uvmap_iccin.o uvmap_add.o EG_uvmapFindUV.o uvmap_struct_tasks.o uvmap_bnd_adj.o EG_uvmapStructFree.o uvmap_inibe.o uvmap_norm_uv.o uvmap_test.o uvmap_mben_disc.o uvmap_find_uv.o uvmap_solve.o uvmap_from_egads.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g -o ./uvmap.exe ./uvmap.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a fgadsBase.o fgadsMemory.o fgadsAttrs.o fgadsTess.o fgadsHLevel.o fgadsGeom.o fgadsTopo.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 ../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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -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=7.7 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
-lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.7.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKSTEP -lTKSTEP209 -lTKSTEPBase -lTKSTEPAttr -lTKXSBase -lTKIGES -lTKFillet -pthread -lm \
-lpthread -lz -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udfWarp.c -o ./udfWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/warp.so ./udfWarp.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. udpNaca456.c -o ./udpNaca456.o
gfortran -g -c -O -fPIC -frecursive -fcray-pointer naca456.f90 -o ./naca456.o -J .
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads \
-lpthread -lz -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/mset
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
gcc -g -o ./hsmTest ./hsmTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
gcc -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
gcc -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
gcc -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
gcc -g -o ./interferenceTest ./interferenceTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
gcc -g -o ./mystranTest ./mystranTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
gfortran -g -c -O -fPIC -frecursive -fcray-pointer friction_eja_mod.f -o ./friction.o
gfortran -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/friction ./friction.o
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm -lpthread
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
Not compiling aflr2AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
Not compiling aflr4AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils su2_801_Harrier.c \
-o ./su2_801_Harrier.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
Not compiling sierraSDAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/plato'
Not compiling platoAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I. -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils -I../meshWriter/fastWriter cbaeroAIM.c -o cbaeroAIM.o
gcc -g -shared -Wl,-no-undefined cbaeroAIM.o -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I../include -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for `default'.
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C cart3d
make[2]: xml2-config: Command not found
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
Not compiling aflr3AIM: AFLR must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
Not compiling sierraSMAIM: SEACAS must be set -- Please fix the environment....
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 \
-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=7.7 \
-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmglr.f -o ./hsmglr.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbc.f -o ./hsmbc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmbb2.f -o ./hsmbb2.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmre1.f -o ./hsmre1.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmdep.f -o ./hsmdep.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmrfm.f -o ./hsmrfm.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmout.f -o ./hsmout.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmren.f -o ./hsmren.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmprj.f -o ./hsmprj.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero atanc.f -o ./atanc.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero cross.f -o ./cross.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero ludcmp.f -o ./ludcmp.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmabd.f -o ./hsmabd.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero bmdump.f -o ./bmdump.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero -fno-recursive hsmrun.f -o ./hsmrun.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmeqn.f -o ./hsmeqn.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmsol.f -o ./hsmsol.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero hsmgeo.f -o ./hsmgeo.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
gfortran -g -c -O -fPIC -frecursive -fcray-pointer -fdefault-real-8 -fbounds-check -ffpe-trap=invalid,zero sbsolve.f -o ./sbsolve.o
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/hsmAIM.so \
src/hsmAIM.o src/hsmUtils.o src/hsmAdj.o \
src/rcm.o src/genrcmi.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -lstdc++
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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_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_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_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_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_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_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_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_VM.c -o avlRead_VM.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_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_SURF.c -o avlRead_SURF.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/avlAIM.so ./avlAIM.o ./avlRead_ELE.o ./avlRead_DERMATB.o ./avlRead_HINGE.o ./avlRead_BODY.o ./avlRead_CNC.o ./avlRead_TOT.o ./avlRead_DERMATS.o ./avlRead_STRP.o ./avlRead_VM.o ./avlRead_CPOML.o ./avlRead_DERMATM.o ./avlRead_SURF.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for `all'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/zaeroAIM.so ./zaeroAIM.o ./zaeroUtils.o ./zaeroLinearFlutter.o ./zaeroTrim.o ./zaeroTypes.o ./zaeroCards.o ./zaeroGeneral.o ./zaeroGraphical.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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=7.7 -I/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/include -I. -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 timPyscript.c -o ./timPyscript.o
touch /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/lib/pyscript.so ./timPyscript.o -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11 -L/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/src/OpenCSM'
*** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/bin
++ uname -a
+ [[ Linux reynolds-centOS7 3.10.0-1160.108.1.el7.x86_64 #1 SMP Thu Jan 25 16:17:31 UTC 2024 x86_64 x86_64 x86_64 GNU/Linux == *\D\a\r\w\i\n* ]]
+ sed -i 's/.*capsExamples.*/#&/' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/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 0m0.084s
user 0m0.064s
sys 0m0.019s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.437s
user 0m0.598s
sys 0m0.038s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.819s
user 0m4.805s
sys 0m0.157s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.659s
user 0m0.873s
sys 0m0.030s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.610s
user 0m0.888s
sys 0m0.024s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.486s
user 0m0.830s
sys 0m0.024s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/legacy/verify_7.7.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.435s
user 0m5.586s
sys 0m0.147s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/CAPS/verify_7.7.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m28.192s
user 0m47.631s
sys 0m0.472s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/verify_7.7.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.580s
user 0m0.971s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m30.285s
user 1m0.998s
sys 0m2.290s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/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 4 warnings and no verification data
real 0m0.296s
user 0m0.309s
sys 0m0.019s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.756s
user 0m1.037s
sys 0m0.026s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.174s
user 0m0.258s
sys 0m0.019s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/basic/verify_7.7.0/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 0m0.437s
user 0m0.551s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 73 tests in 2.114s
OK
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m6.683s
user 0m12.262s
sys 0m0.150s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 19.806s
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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
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 = 0.065 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 = 0.177 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 = 0.028 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 = 0.100 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.006 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 = 0.057 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 = 0.107 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 = 0.028 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 = 0.100 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.032 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 = 0.030 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 = 0.097 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.008 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 = 0.000 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 190 332
AFLR2 : CPU Time = 0.000 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 190
Number of elements = 380
Number of tris = 332
Number of quad = 0
ok
test_reenter (test_aflr2.TestAFLR2.test_reenter) ... Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 5
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = TunnelWall, index = 1
Name = OutFlow, index = 2
Name = InFlow, index = 3
Name = Airfoil, index = 4
Getting mesh sizing parameters
Mesh sizing name - 2DSlice
Mesh sizing name - Airfoil
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting 2D mesh for body 1 (of 1)
AFLR2 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 = 0.009 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.001 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
SU2 expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing SU2 file
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 = 0.014 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 = 0.008 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 ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
libMeshb expects 2D meshes in the x-y plane... attempting to rotate mesh!Swapping z and y coordinates!
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK 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
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 = 0.001 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 = 0.014 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 = 0.008 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:63376)
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:42PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 6092
Number of elements = 33723
Number of triangles = 4434
Number of quadrilatarals = 0
Number of tetrahedrals = 29289
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 13578
Number of elements = 76165
Number of triangles = 8144
Number of quadrilatarals = 0
Number of tetrahedrals = 68021
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 42341
Number of elements = 240656
Number of triangles = 19890
Number of quadrilatarals = 0
Number of tetrahedrals = 220766
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 4356
Number of elements = 24173
Number of triangles = 3018
Number of quadrilatarals = 0
Number of tetrahedrals = 21155
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 10984
Number of elements = 60667
Number of triangles = 8628
Number of quadrilatarals = 0
Number of tetrahedrals = 52039
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 10678
Number of elements = 59894
Number of triangles = 6366
Number of quadrilatarals = 0
Number of tetrahedrals = 53528
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 89218
Number of elements = 501527
Number of triangles = 51812
Number of quadrilatarals = 0
Number of tetrahedrals = 449715
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:63376)
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 17611
Number of elements = 100342
Number of triangles = 8270
Number of quadrilatarals = 0
Number of tetrahedrals = 92072
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3649
Number of elements = 19777
Number of triangles = 3394
Number of quadrilatarals = 0
Number of tetrahedrals = 16383
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5514
Number of elements = 30658
Number of triangles = 3656
Number of quadrilatarals = 0
Number of tetrahedrals = 27002
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1494
Number of elements = 7708
Number of triangles = 1988
Number of quadrilatarals = 0
Number of tetrahedrals = 5720
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1558
Number of elements = 7832
Number of triangles = 2112
Number of quadrilatarals = 0
Number of tetrahedrals = 5720
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1151
Number of elements = 6028
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4720
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 363
Number of elements = 1645
Number of triangles = 720
Number of quadrilatarals = 0
Number of tetrahedrals = 925
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5092
Number of elements = 27888
Number of triangles = 4070
Number of quadrilatarals = 0
Number of tetrahedrals = 23818
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5238
Number of elements = 28440
Number of triangles = 4622
Number of quadrilatarals = 0
Number of tetrahedrals = 23818
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 4902
Number of elements = 26933
Number of triangles = 4038
Number of quadrilatarals = 0
Number of tetrahedrals = 22895
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 33106
Number of elements = 191761
Number of triangles = 8496
Number of quadrilatarals = 0
Number of tetrahedrals = 183265
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 36447
Number of elements = 205093
Number of triangles = 21828
Number of quadrilatarals = 0
Number of tetrahedrals = 183265
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 28882
Number of elements = 164134
Number of triangles = 15162
Number of quadrilatarals = 0
Number of tetrahedrals = 148972
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 4186
Number of elements = 23181
Number of triangles = 2942
Number of quadrilatarals = 0
Number of tetrahedrals = 20239
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16786
Number of elements = 95215
Number of triangles = 8798
Number of quadrilatarals = 0
Number of tetrahedrals = 86417
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18710
Number of elements = 102591
Number of triangles = 16174
Number of quadrilatarals = 0
Number of tetrahedrals = 86417
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 12124
Number of elements = 68112
Number of triangles = 7138
Number of quadrilatarals = 0
Number of tetrahedrals = 60974
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 6586
Number of elements = 34479
Number of triangles = 9036
Number of quadrilatarals = 0
Number of tetrahedrals = 25443
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20591
Number of elements = 119086
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 113640
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18187
Number of elements = 104960
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 99704
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20591
Number of elements = 119086
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 113640
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18187
Number of elements = 104960
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 99704
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20591
Number of elements = 119086
Number of triangles = 5446
Number of quadrilatarals = 0
Number of tetrahedrals = 113640
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 18187
Number of elements = 104960
Number of triangles = 5256
Number of quadrilatarals = 0
Number of tetrahedrals = 99704
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_quad (test_aflr3.TestAFLR3.test_quad) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 28277
Number of elements = 127463
Number of triangles = 410
Number of quadrilatarals = 3218
Number of tetrahedrals = 116651
Number of pyramids = 0
Number of prisms = 748
Number of hexahedrals = 6436
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing SU2 file ....
Finished writing SU2 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 20346
Number of elements = 117776
Number of triangles = 5542
Number of quadrilatarals = 0
Number of tetrahedrals = 112234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 17847
Number of elements = 102603
Number of triangles = 5384
Number of quadrilatarals = 0
Number of tetrahedrals = 97219
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6342
Number of elements = 35410
Number of triangles = 4052
Number of quadrilatarals = 0
Number of tetrahedrals = 31358
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 41941
Number of elements = 242460
Number of triangles = 11826
Number of quadrilatarals = 0
Number of tetrahedrals = 230634
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 45637
Number of elements = 264476
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 252780
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 41941
Number of elements = 242330
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 230634
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
test_Edge_scaleFactor (test_aflr4.TestAFLR4.test_Edge_scaleFactor) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_Face_scaleFactor (test_aflr4.TestAFLR4.test_Face_scaleFactor) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leftWing
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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_erw (test_aflr4.TestAFLR4.test_erw) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - leftWing
Done getting mesh sizing parameters
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_ff_cdfr (test_aflr4.TestAFLR4.test_ff_cdfr) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
ok
test_max_min_scale (test_aflr4.TestAFLR4.test_max_min_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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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_proximity (test_aflr4.TestAFLR4.test_proximity) ... 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 - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
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 - Wing1
Mesh sizing name - Wing2
Done getting mesh sizing parameters
ok
test_quad (test_aflr4.TestAFLR4.test_quad) ... 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing SU2 file ....
Finished writing SU2 file
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 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 ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: box
2: cut
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
ok
test_setInput (test_aflr4.TestAFLR4.test_setInput) ... ok
test_skin (test_aflr4.TestAFLR4.test_skin) ... 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 ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid 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 Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
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_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) ... skipped 'No flowCart executable'
test_outputs (test_cart3d.TestCart3D.test_outputs) ... skipped 'No flowCart executable'
test_reenter (test_cart3d.TestCart3D.test_reenter) ... skipped 'No flowCart executable'
test_sensitivity_AnalysisIn (test_cart3d.TestCart3D.test_sensitivity_AnalysisIn) ... skipped 'No flowCart executable'
test_sensitivity_GeometryIn (test_cart3d.TestCart3D.test_sensitivity_GeometryIn) ... skipped 'No flowCart executable'
test_Output_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 = 3
Name = riteWing, index = 1
Name = leftWing, index = 2
Name = trailingEdge, index = 3
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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:63376)
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
7FDEDBFFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FDEDBFFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FDF0A494740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FDF0A494740 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
7FDEE8906700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FDEE8906700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FDEE9107700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FDEE9107700 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
7FDEE8906700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FDEE8906700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FDEDBFFF700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FDEDBFFF700 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
7FDEDBFFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FDEDBFFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FDF0A494740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FDF0A494740 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:63376)
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:63376)
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:63376)
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:63376)
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:63376)
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:63376)
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
Writing vtk file ....
Writing vtk surface file ....
capsGroups found:
1: Farfield
2: Wing1
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 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 = 6733
Number of elements = 13462
Number of triangle elements = 13462
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 4939
Number of elements = 9874
Number of triangle elements = 9874
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 194
Number of elements = 384
Number of triangle elements = 384
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11866
Total number of elements = 23720
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 - 11866, elements - 23720
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.19
Creating surface mesh ...
Surface mesh seconds: 0.04
Recovering boundaries...
Boundary recovery seconds: 0.14
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.07
Recovering Delaunayness...
Delaunay recovery seconds: 0.09
Refining mesh...
15817 insertions, added 8303 points, 522536 tetrahedra in queue.
5267 insertions, added 1663 points, 527861 tetrahedra in queue.
7020 insertions, added 1641 points, 485124 tetrahedra in queue.
9358 insertions, added 1385 points, 317076 tetrahedra in queue.
12474 insertions, added 1249 points, 13147 tetrahedra in queue.
16628 insertions, added 1732 points, 22447 tetrahedra in queue.
Refinement seconds: 7.93
Smoothing vertices...
Mesh smoothing seconds: 2.72
Improving mesh...
Mesh improvement seconds: 0.07
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.02
Total running seconds: 11.27
Statistics:
Input points: 11866
Input facets: 23720
Input segments: 35580
Input holes: 2
Input regions: 0
Mesh points: 28570
Mesh tetrahedra: 138560
Mesh faces: 288980
Mesh faces on exterior boundary: 23720
Mesh faces on input facets: 23720
Mesh edges on input segments: 35580
Steiner points inside domain: 16704
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 = 6733
Number of elements = 13462
Number of triangle elements = 13462
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 4939
Number of elements = 9874
Number of triangle elements = 9874
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 194
Number of elements = 384
Number of triangle elements = 384
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 11866
Total number of elements = 23720
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 - 11866, elements - 23720
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.13
Creating surface mesh ...
Surface mesh seconds: 0.04
Recovering boundaries...
Boundary recovery seconds: 0.14
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.06
Recovering Delaunayness...
Delaunay recovery seconds: 0.06
Refining mesh...
15817 insertions, added 8303 points, 522536 tetrahedra in queue.
5267 insertions, added 1663 points, 527861 tetrahedra in queue.
7020 insertions, added 1641 points, 485124 tetrahedra in queue.
9358 insertions, added 1385 points, 317076 tetrahedra in queue.
12474 insertions, added 1249 points, 13147 tetrahedra in queue.
16628 insertions, added 1732 points, 22447 tetrahedra in queue.
Refinement seconds: 7.88
Smoothing vertices...
Mesh smoothing seconds: 2.51
Improving mesh...
Mesh improvement seconds: 0.06
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.02
Total running seconds: 10.9
Statistics:
Input points: 11866
Input facets: 23720
Input segments: 35580
Input holes: 2
Input regions: 0
Mesh points: 28570
Mesh tetrahedra: 138560
Mesh faces: 288980
Mesh faces on exterior boundary: 23720
Mesh faces on input facets: 23720
Mesh edges on input segments: 35580
Steiner points inside domain: 16704
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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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)
/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 - 1206, elements - 2400
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 - 1206, elements - 2400
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 - 11866, elements - 23720
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... skipped 'No pointwise executable'
test_SingleBody (test_pointwise.TestPointwise.test_SingleBody) ... skipped 'No pointwise executable'
test_all (test_pointwise.TestPointwise.test_all) ... skipped 'No pointwise executable'
test_box (test_pointwise.TestPointwise.test_box) ... skipped 'No pointwise executable'
test_bullet (test_pointwise.TestPointwise.test_bullet) ... skipped 'No pointwise executable'
test_cone (test_pointwise.TestPointwise.test_cone) ... skipped 'No pointwise executable'
test_cylinder (test_pointwise.TestPointwise.test_cylinder) ... skipped 'No pointwise executable'
test_executeError (test_pointwise.TestPointwise.test_executeError) ... skipped 'No pointwise executable'
test_reenter (test_pointwise.TestPointwise.test_reenter) ... skipped 'No pointwise executable'
test_sphere (test_pointwise.TestPointwise.test_sphere) ... skipped 'No pointwise executable'
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
test_Area_Mesh (test_refine.TestREFINE.test_Area_Mesh) ... skipped "No 'ref' executable"
test_all (test_refine.TestREFINE.test_all) ... skipped "No 'ref' executable"
test_box_volume (test_refine.TestREFINE.test_box_volume) ... skipped "No 'ref' executable"
test_boxhole (test_refine.TestREFINE.test_boxhole) ... skipped "No 'ref' executable"
test_cfdSingleBody (test_refine.TestREFINE.test_cfdSingleBody) ... skipped "No 'ref' executable"
test_fun3d (test_refine.TestREFINE.test_fun3d) ... skipped "No 'ref' executable"
test_inputs (test_refine.TestREFINE.test_inputs) ... skipped "No 'ref' executable"
test_phase (test_refine.TestREFINE.test_phase) ... skipped "No 'ref' executable"
test_sphere (test_refine.TestREFINE.test_sphere) ... skipped "No 'ref' executable"
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
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 7.7.0
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 15.2802204 0 0.00183652568
EGADS : 11 Yes 16.1331862 2.82842712 0
EGADS : 12 Yes 13.7712362 0 0
EGADS : 13 Yes 15.4042293 2.82842712 0.0493703791
EGADS : 14 Yes 15.2792409 0 0
EGADS : 15 Yes 16.1323663 2.82842712 0
EGADS : 16 Yes 16.1331862 0 0
EGADS : 17 Yes 15.4042293 0 0.0493703791
EGADS : 18 Yes 16.1323663 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 = 16.1372
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 14.7419
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= 11696
AFLR43 : Nodes = 5854
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 = 5854 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 = 0.014 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 5854 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1172 6979
AFLR3 IG : Nodes, Elements = 2344 15144
AFLR3 IG : Nodes, Elements = 3516 23433
AFLR3 IG : Nodes, Elements = 4688 31724
AFLR3 IG : Nodes, Elements = 5860 39971
AFLR3 IG : Nodes, Elements = 5861 39981
AFLR3 IG : Nodes, Elements = 5861 39927
AFLR3 IG : Nodes, Elements = 5861 39953
AFLR3 IG : Nodes, Elements = 5861 39924
AFLR3 IG : Nodes, Elements = 5854 23729
AFLR3 IG : Nodes, Elements = 5854 23747
AFLR3 IG : Nodes, Elements = 5854 19648
AFLR3 IG : Nodes, Elements = 5854 17671
AFLR3 : CPU Time = 0.165 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 5854 17671
AFLR3 GG : Nodes, Elements = 8503 25816
AFLR3 GG : Nodes, Elements = 8503 37060
AFLR3 GG : Nodes, Elements = 8503 34199
AFLR3 GG : Nodes, Elements = 8503 32662
AFLR3 GG : Nodes, Elements = 10841 40059
AFLR3 GG : Nodes, Elements = 10841 50115
AFLR3 GG : Nodes, Elements = 10841 47116
AFLR3 GG : Nodes, Elements = 10841 46256
AFLR3 GG : Nodes, Elements = 13334 54007
AFLR3 GG : Nodes, Elements = 13334 65003
AFLR3 GG : Nodes, Elements = 13334 61748
AFLR3 GG : Nodes, Elements = 13334 60928
AFLR3 GG : Nodes, Elements = 16071 69303
AFLR3 GG : Nodes, Elements = 16071 81240
AFLR3 GG : Nodes, Elements = 16071 77929
AFLR3 GG : Nodes, Elements = 16071 77128
AFLR3 GG : Nodes, Elements = 18948 85925
AFLR3 GG : Nodes, Elements = 18948 98362
AFLR3 GG : Nodes, Elements = 18948 94962
AFLR3 GG : Nodes, Elements = 18948 94173
AFLR3 GG : Nodes, Elements = 21901 103180
AFLR3 GG : Nodes, Elements = 21901 116113
AFLR3 GG : Nodes, Elements = 21901 112513
AFLR3 GG : Nodes, Elements = 21901 111676
AFLR3 GG : Nodes, Elements = 24998 121128
AFLR3 GG : Nodes, Elements = 24998 134436
AFLR3 GG : Nodes, Elements = 24998 130836
AFLR3 GG : Nodes, Elements = 24998 129947
AFLR3 GG : Nodes, Elements = 28191 139639
AFLR3 GG : Nodes, Elements = 28191 153349
AFLR3 GG : Nodes, Elements = 28191 149657
AFLR3 GG : Nodes, Elements = 28191 148882
AFLR3 GG : Nodes, Elements = 31447 158756
AFLR3 GG : Nodes, Elements = 31447 172634
AFLR3 GG : Nodes, Elements = 31447 169045
AFLR3 GG : Nodes, Elements = 31447 168284
AFLR3 GG : Nodes, Elements = 34739 178244
AFLR3 GG : Nodes, Elements = 34739 192267
AFLR3 GG : Nodes, Elements = 34739 188516
AFLR3 GG : Nodes, Elements = 34739 187746
AFLR3 GG : Nodes, Elements = 38006 197599
AFLR3 GG : Nodes, Elements = 38006 211318
AFLR3 GG : Nodes, Elements = 38006 207734
AFLR3 GG : Nodes, Elements = 38006 207079
AFLR3 GG : Nodes, Elements = 41126 216478
AFLR3 GG : Nodes, Elements = 41126 229785
AFLR3 GG : Nodes, Elements = 41126 226344
AFLR3 GG : Nodes, Elements = 41126 225710
AFLR3 GG : Nodes, Elements = 44145 234801
AFLR3 GG : Nodes, Elements = 44145 247555
AFLR3 GG : Nodes, Elements = 44145 244361
AFLR3 GG : Nodes, Elements = 44145 243762
AFLR3 GG : Nodes, Elements = 47047 252497
AFLR3 GG : Nodes, Elements = 47047 264690
AFLR3 GG : Nodes, Elements = 47047 261507
AFLR3 GG : Nodes, Elements = 47047 260955
AFLR3 GG : Nodes, Elements = 49854 269397
AFLR3 GG : Nodes, Elements = 49854 281243
AFLR3 GG : Nodes, Elements = 49854 278226
AFLR3 GG : Nodes, Elements = 49854 277712
AFLR3 GG : Nodes, Elements = 52533 285757
AFLR3 GG : Nodes, Elements = 52533 297092
AFLR3 GG : Nodes, Elements = 52533 294178
AFLR3 GG : Nodes, Elements = 52533 293714
AFLR3 GG : Nodes, Elements = 55049 301265
AFLR3 GG : Nodes, Elements = 55049 311812
AFLR3 GG : Nodes, Elements = 55049 309171
AFLR3 GG : Nodes, Elements = 55049 308736
AFLR3 GG : Nodes, Elements = 57409 315819
AFLR3 GG : Nodes, Elements = 57409 325733
AFLR3 GG : Nodes, Elements = 57409 323182
AFLR3 GG : Nodes, Elements = 57409 322836
AFLR3 GG : Nodes, Elements = 59614 329454
AFLR3 GG : Nodes, Elements = 59614 338622
AFLR3 GG : Nodes, Elements = 59614 336360
AFLR3 GG : Nodes, Elements = 59614 336020
AFLR3 GG : Nodes, Elements = 61594 341962
AFLR3 GG : Nodes, Elements = 61594 350315
AFLR3 GG : Nodes, Elements = 61594 348166
AFLR3 GG : Nodes, Elements = 61594 347938
AFLR3 GG : Nodes, Elements = 63311 353092
AFLR3 GG : Nodes, Elements = 63311 360277
AFLR3 GG : Nodes, Elements = 63311 358448
AFLR3 GG : Nodes, Elements = 63311 358215
AFLR3 GG : Nodes, Elements = 64762 362570
AFLR3 GG : Nodes, Elements = 64762 368558
AFLR3 GG : Nodes, Elements = 64762 367047
AFLR3 GG : Nodes, Elements = 64762 366877
AFLR3 GG : Nodes, Elements = 65935 370396
AFLR3 GG : Nodes, Elements = 65935 375299
AFLR3 GG : Nodes, Elements = 65935 374006
AFLR3 GG : Nodes, Elements = 65935 373889
AFLR3 GG : Nodes, Elements = 66772 376401
AFLR3 GG : Nodes, Elements = 66772 379936
AFLR3 GG : Nodes, Elements = 66772 378979
AFLR3 GG : Nodes, Elements = 66772 378887
AFLR3 GG : Nodes, Elements = 67334 380573
AFLR3 GG : Nodes, Elements = 67334 382968
AFLR3 GG : Nodes, Elements = 67334 382266
AFLR3 GG : Nodes, Elements = 67334 382222
AFLR3 GG : Nodes, Elements = 67728 383404
AFLR3 GG : Nodes, Elements = 67728 385074
AFLR3 GG : Nodes, Elements = 67728 384601
AFLR3 GG : Nodes, Elements = 67728 384568
AFLR3 GG : Nodes, Elements = 67984 385336
AFLR3 GG : Nodes, Elements = 67984 386402
AFLR3 GG : Nodes, Elements = 67984 386107
AFLR3 GG : Nodes, Elements = 67984 386081
AFLR3 GG : Nodes, Elements = 68134 386533
AFLR3 GG : Nodes, Elements = 68134 387183
AFLR3 GG : Nodes, Elements = 68134 386980
AFLR3 GG : Nodes, Elements = 68134 386962
AFLR3 GG : Nodes, Elements = 68226 387238
AFLR3 GG : Nodes, Elements = 68226 387592
AFLR3 GG : Nodes, Elements = 68226 387510
AFLR3 GG : Nodes, Elements = 68226 387507
AFLR3 GG : Nodes, Elements = 68276 387657
AFLR3 GG : Nodes, Elements = 68276 387861
AFLR3 GG : Nodes, Elements = 68276 387804
AFLR3 GG : Nodes, Elements = 68276 387797
AFLR3 GG : Nodes, Elements = 68304 387881
AFLR3 GG : Nodes, Elements = 68304 387999
AFLR3 GG : Nodes, Elements = 68304 387963
AFLR3 GG : Nodes, Elements = 68304 387961
AFLR3 GG : Nodes, Elements = 68320 388009
AFLR3 GG : Nodes, Elements = 68320 388078
AFLR3 GG : Nodes, Elements = 68320 388056
AFLR3 GG : Nodes, Elements = 68330 388086
AFLR3 GG : Nodes, Elements = 68330 388124
AFLR3 GG : Nodes, Elements = 68330 388114
AFLR3 GG : Nodes, Elements = 68330 388113
AFLR3 GG : Nodes, Elements = 68339 388140
AFLR3 GG : Nodes, Elements = 68339 388170
AFLR3 GG : Nodes, Elements = 68339 388165
AFLR3 GG : Nodes, Elements = 68345 388183
AFLR3 GG : Nodes, Elements = 68345 388210
AFLR3 GG : Nodes, Elements = 68345 388201
AFLR3 GG : Nodes, Elements = 68348 388210
AFLR3 GG : Nodes, Elements = 68348 388221
AFLR3 GG : Nodes, Elements = 68348 388219
AFLR3 GG : Nodes, Elements = 68349 388222
AFLR3 GG : Nodes, Elements = 68349 388225
AFLR3 GG : Nodes, Elements = 68350 388228
AFLR3 GG : Nodes, Elements = 68350 388231
AFLR3 GG : Nodes, Elements = 68350 388230
AFLR3 GG : Nodes, Elements = 68369 388287
AFLR3 GG : Nodes, Elements = 68369 388368
AFLR3 GG : Nodes, Elements = 68369 388339
AFLR3 GG : Nodes, Elements = 68369 388335
AFLR3 GG : Nodes, Elements = 68373 388347
AFLR3 GG : Nodes, Elements = 68373 388364
AFLR3 GG : Nodes, Elements = 68373 388359
AFLR3 GG : Nodes, Elements = 68373 388358
AFLR3 GG : Nodes, Elements = 68374 388361
AFLR3 GG : Nodes, Elements = 68374 388366
AFLR3 GG : Nodes, Elements = 68374 388365
AFLR3 GG : Nodes, Elements = 68374 388363
AFLR3 : CPU Time = 6.488 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 68374 388363
AFLR3 QI : Nodes, Elements = 66929 380164
AFLR3 QI : Nodes, Elements = 66695 378855
AFLR3 QI : Nodes, Elements = 66670 378717
AFLR3 QI : Nodes, Elements = 66668 378707
AFLR3 QI : Nodes, Elements = 66668 382418
AFLR3 QI : Nodes, Elements = 66668 378435
AFLR3 QI : Nodes, Elements = 66668 378010
AFLR3 QI : Nodes, Elements = 66668 380528
AFLR3 QI : Nodes, Elements = 66668 378087
AFLR3 QI : Nodes, Elements = 66668 377980
AFLR3 QI : Nodes, Elements = 66668 378646
AFLR3 QI : Nodes, Elements = 66668 377861
AFLR3 QI : Nodes, Elements = 66668 377723
AFLR3 QI : Nodes, Elements = 66668 378078
AFLR3 QI : Nodes, Elements = 66668 377689
AFLR3 QI : Nodes, Elements = 66668 377615
AFLR3 QI : Nodes, Elements = 66668 377954
AFLR3 QI : Nodes, Elements = 66668 377630
AFLR3 QI : Nodes, Elements = 66668 377605
AFLR3 QI : Nodes, Elements = 66674 377631
AFLR3 QI : Nodes, Elements = 66674 377980
AFLR3 QI : Nodes, Elements = 66674 377664
AFLR3 QI : Nodes, Elements = 66674 377639
AFLR3 QI : Nodes, Elements = 66674 377938
AFLR3 QI : Nodes, Elements = 66674 377653
AFLR3 QI : Nodes, Elements = 66674 377609
AFLR3 QI : Nodes, Elements = 66674 377631
AFLR3 : CPU Time = 2.570 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 66674 377631
AFLR3 QRG: Nodes, Elements = 66680 377670
AFLR3 QRG: Nodes, Elements = 66695 377754
AFLR3 QRG: Nodes, Elements = 66694 377749
AFLR3 QRG: Nodes, Elements = 66695 377753
AFLR3 QRG: Nodes, Elements = 66695 377752
AFLR3 QRG: Nodes, Elements = 66699 377777
AFLR3 QRG: Nodes, Elements = 66709 377830
AFLR3 : CPU Time = 0.069 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 377830
UG3 : Min, Max Ang = 0.9631 175.1
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 160
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 377830
UG3 : Min Vol = 6.55e-10
UG3 : Average Vol = 5.62
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 = 377830
UG3 : Min, Max Q = 0.0742 1
UG3 : Average Q = 0.886
UG3 : No. Q< 0.1 = 26
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 10.012 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 377830
UG3 : Min, Max Ang = 0.9631 175.1
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 160
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 377830
UG3 : Min Vol = 6.55e-10
UG3 : Average Vol = 5.62
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 = 377830
UG3 : Min, Max Q = 0.142 1
UG3 : Average Q = 0.863
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
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 = 66709
Number of elements = 389526
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 377830
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 66709
Number of elements = 389526
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 377830
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 66709
Number of elements = 389526
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 377830
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 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 66709
Number of elements = 389526
Number of triangles = 11696
Number of quadrilatarals = 0
Number of tetrahedrals = 377830
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:63376)
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)
7FDEE9107700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FDEDBFFF700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FDEDBFFF700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
7FDEE9107700 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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!
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 - 5857, elements - 11706
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 = 4
Name = Farfield, index = 1
Name = riteWing, index = 2
Name = leftWing, index = 3
Name = trailingEdge, index = 4
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 = 7130
Number of elements = 14252
Number of triangle elements = 14252
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7130
Total number of elements = 14252
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!
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 file
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 = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing ASCII STL file ....
Finished writing ASCII STL file
Writing Binary STL file ....
Finished writing Binary STL file
Writing Tecplot file ....
Finished writing Tecplot file
Writing vtk file ....
Writing vtk general file ....
Finished writing vtk file
Writing Binary VTK file ....
Finished writing Binary VTK file
Writing FAST file ....
Finished writing FAST file
Writing SU2 file ....
Finished writing SU2 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_Cl (test_xfoil.Testxfoil_Parsec.test_Cl) ... ok
test_alpha_custom_increment (test_xfoil.Testxfoil_Parsec.test_alpha_custom_increment) ... 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 154 tests in 603.667s
OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `avlTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `awaveTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `frictionTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for `fun3d'.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `hsm' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `interferenceTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `msesTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `mystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `pointwiseTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(cd ./regressionTest; ./execute_CTestRegression.sh MINIMAL)
Running.... MINIMAL c-Tests
All tests pass!
(cd ./regressionTest; ./execute_PyTestRegression.sh MINIMAL)
=================================================
Using python : /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0.0006119078685746836
CYtot -6.288067668554914e-15
CZtot -0.3012861394886091
Cltot -4.782099331324466e-14
Cmtot -0.1945055953450467
Cntot -2.339543963831951e-15
Cl'tot -4.785454061647156e-14
Cn'tot -1.504596228417061e-15
CLtot 0.3012509314150772
CDtot 0.004646353488232841
CDvis 0.0
CLff 0.3009503023520527
CYff -7.718708857566269e-15
CDind 0.004646353488232841
CDff 0.004968969500908292
e 0.9669902146157957
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 0m0.741s
user 0m0.544s
sys 0m0.409s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'xfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
Cl = [1.05475230552567, 1.36488869373635, 1.56607214272105, 2.03059709344862, 1.97271083121169, 1.87307153172386, 1.76050475760117]
Cd = [0.0131991208675727, 0.0166540240605751, 0.0200551482562831, 0.0458671341969345, 0.0754256009394856, 0.0994469174477522, 0.127479430989037]
Alpha = [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location = [0.4960441144043, 0.461377732041502, 0.44237656820185, 0.361251636355465, 0.276104140853559, 0.214381239321467, 0.132988264746661]
real 0m4.824s
user 0m4.681s
sys 0m0.355s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'mses_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
mses_PyTest.py test;
+ python -u mses_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837910855492407
Cd = 0.007775858417210143
Cm = 0.005262636995811319
real 0m5.384s
user 0m5.235s
sys 0m0.366s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case mses_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'friction_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0m0.609s
user 0m0.469s
sys 0m0.345s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tsfoil_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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.
Cl = 0.933329
Cd = 0.000283
Cd Wave = 0.0
Cm = -0.203433
Cp _Critcal = -1.303869
real 0m0.637s
user 0m0.584s
sys 0m0.324s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tsfoil_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'delaundo_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u delaundo_PyTest.py -outLevel=0
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 0m0.767s
user 0m0.702s
sys 0m0.481s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case delaundo_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'egadsTess_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0m6.520s
user 0m13.666s
sys 0m1.317s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case egadsTess_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
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 = 0.012 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 0m0.794s
user 0m0.830s
sys 0m0.395s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'aflr4_and_aflr3_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr4_and_aflr3_PyTest.py test;
+ python -u aflr4_and_aflr3_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
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 11.5.15
AFLR4 : Version Date 07/19/24 @ 07:04PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 07/19/24 @ 07:42PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.26
EGADS : OpenCASCADE Version 7.7.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 151604
Number of elements = 458324
Number of triangles = 14380
Number of quadrilatarals = 0
Number of tetrahedrals = 222892
Number of pyramids = 425
Number of prisms = 220627
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
real 0m16.297s
user 0m15.994s
sys 0m0.481s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case aflr4_and_aflr3_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'tetgen_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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: 0.02
Creating surface mesh ...
Surface mesh seconds: 0.01
Recovering boundaries...
Boundary recovery seconds: 0.06
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.01
Suppressing Steiner points ...
Steiner suppression seconds: 0
Recovering Delaunayness...
Delaunay recovery seconds: 0.01
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: 0.79
Smoothing vertices...
Mesh smoothing seconds: 0.5
Improving mesh...
Mesh improvement seconds: 0.01
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.01
Total running seconds: 1.42
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 0m2.865s
user 0m2.923s
sys 0m0.363s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case tetgen_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'su2_and_AFLR2_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
su2_and_AFLR2_PyTest.py test;
+ python -u su2_and_AFLR2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 9.18.1
AFLR2 : Version Date 06/11/24 @ 05:52PM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 06/11/24 @ 06:33PM
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 = 0.045 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 = 0.017 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| 1.0897e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0746e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0676e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0573e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0564e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.0525e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.0489e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0501e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0463e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0413e-01| -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 0m2.215s
user 0m2.073s
sys 0m0.533s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case su2_and_AFLR2_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'masstran_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0m4.519s
user 0m7.291s
sys 0m1.604s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case masstran_PyTest.py passed (as expected)
=================================================
=================================================
+ echo 'hsm_SingleLoadCase_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
hsm_SingleLoadCase_PyTest.py test;
+ python -u hsm_SingleLoadCase_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0.19 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 0.19 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 0.848E-15 0.147E-13 0.924E-15 1.000 ddy @ ( 0.25 0.19 0.00)
Converging n vectors ...
it = 1 dn = 0.788E-01 rlx = 1.000 ( 59 )
it = 2 dn = 0.566E-16 rlx = 1.000 ( 35 )
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 0m1.543s
user 0m1.483s
sys 0m0.270s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case hsm_SingleLoadCase_PyTest.py passed (as expected)
=================================================
=================================================
+ echo '../corsairlite/qp.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/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 0m2.379s
user 0m2.483s
sys 0m0.596s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case ../corsairlite/qp.py passed (as expected)
=================================================
*************************************************
*************************************************
=================================================
Did not run examples for:
abaqus
awave
Cart3D
Astros
Mystran
=================================================
All tests pass!
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/test/plugs
+ find /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
find: ‘/home/jenkins/workspace/ESP_Beta/7.7/LINUX64/EngSketchPad/data/Plugs’: No such file or directory
+ awk '{ n=split($0, a, ";"); for(i=1; i<=n; i+=2) print a[i] }' /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.7/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 28M
-rw-rw-r--. 1 jenkins jenkins 1.3M Jul 26 09:51 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K Jul 26 09:51 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jul 26 09:51 avl
-rwxrwxr-x. 1 jenkins jenkins 29K Jul 26 09:50 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 114K Jul 26 09:52 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins 46K Jul 26 09:52 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M Jul 26 09:51 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K Jul 26 09:51 mses
-rwxrwxr-x. 1 jenkins jenkins 536K Jul 26 09:51 mset
-rwxrwxr-x. 1 jenkins jenkins 39K Jul 26 09:51 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K Jul 26 09:54 pod.egads
-rw-rw-r--. 1 jenkins jenkins 0 Jul 26 09:54 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K Jul 26 09:51 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K Jul 26 09:51 pxplot
-rwxrwxr-x. 1 jenkins jenkins 115K Jul 26 09:51 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 507K Jul 26 09:51 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 458K Jul 26 09:51 serveESP
-rwxrwxr-x. 1 jenkins jenkins 568K Jul 26 09:51 Slugs
-rwxrwxr-x. 1 jenkins jenkins 169K Jul 26 09:51 TestFit
-rwxrwxr-x. 1 jenkins jenkins 62K Jul 26 09:50 vCurvature
-rwxrwxr-x. 1 jenkins jenkins 36K Jul 26 09:50 vGeom
-rwxrwxr-x. 1 jenkins jenkins 63K Jul 26 09:50 vTess
-rwxrwxr-x. 1 jenkins jenkins 12M Jul 26 09:50 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 197K Jul 26 09:54 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M Jul 26 09:51 xfoil
[Execution node] check if [reynolds-centOS7] is in [[viggen]]
Run condition [Execution node ] preventing perform for step [Execute shell]
[Execution node] check if [reynolds-centOS7] is in [[windows10x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
[GNU C Compiler (gcc)] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[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: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[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: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Skipping post processing
[Static Analysis] No filter has been set, publishing all 0 issues
[Static Analysis] Repository miner is not configured, skipping repository mining
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.7/LINUX64')
[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=7.7,ESP_ARCH=LINUX64,buildnode=reynolds-centOS7 #739'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS