Started by upstream project "ESP_Beta" build number 720
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/7.8/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/7.8/LINUX64
Cleaning local Directory .
Checking out svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins at revision '2024-05-30T12:18:09.796 -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 2501
Checking out a fresh workspace because /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP doesn't exist
Cleaning local Directory JenkinsESP
Checking out svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP at revision '2024-05-30T12:18:09.796 -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 863
No changes for svn+ssh://acdl.mit.edu/home/svnroot/OpenCSM/trunk/Jenkins since the previous build
No changes for svn+ssh://acdl.mit.edu/home/svnroot/JenkinsESP since the previous build
[GitCheckoutListener] SCM 'hudson.scm.SubversionSCM' is not of type GitSCM
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute shell]
Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command]
[Execution node] check if [reynolds-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/jenkins17780152403357341343.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Beta.sh
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/ESP_Env.sh
++ export OCCTREF=7.8
++ OCCTREF=7.8
++ AFLR_VERSION=11.5.14
++ SU2_VERSION=8.0.0
++ TETGEN_VERSION=1.6.0
++ VSP_VERSION=3.38.0
++ export PYTHON_VERSION=3.11.9
++ PYTHON_VERSION=3.11.9
++ export EFCOMP=gfortran
++ EFCOMP=gfortran
++ [[ reynolds-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
++ [[ LINUX64 == \D\A\R\W\I\N\6\4\.\g\c\c ]]
++ export ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_BLOC=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64
++ export JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/julia
++ JULIA_DEPOT_PATH=/home/jenkins/workspace/ESP_Beta/7.8/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-7.8.0
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/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_11.5.14
++ AFLR=/home/jenkins/util/AFLR/aflr_lib_11.5.14
++ export AFLR_ARCH=Linux-x86-64
++ AFLR_ARCH=Linux-x86-64
++ export PATH=/home/jenkins/util/abaqus/DassaultSystemes/SIMULIA/Commands:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/bin:/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/7.8/LINUX64/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ export PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/OpenCSM/trunk/data
++ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/data
+ virtualenv /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv
created virtual environment CPython3.11.9.final.0-64 in 358ms
creator CPython3Posix(dest=/home/jenkins/workspace/ESP_Beta/7.8/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==24.0, setuptools==69.5.1, wheel==0.43.0
activators BashActivator,CShellActivator,FishActivator,NushellActivator,PowerShellActivator,PythonActivator
+ . /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate
++ '[' /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/activate = /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP_venv
++ '[' linux-gnu = cygwin ']'
++ '[' linux-gnu = msys ']'
++ export VIRTUAL_ENV
++ _OLD_VIRTUAL_PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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 (24.0)
+ pip_install f90nml
+ /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade numpy
Collecting numpy
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (61 kB)
Using cached numpy-1.26.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (18.3 MB)
Installing collected packages: numpy
Successfully installed numpy-1.26.4
+ pip_install openmdao
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade openmdao
Collecting openmdao
Using cached openmdao-3.32.0-py3-none-any.whl
Collecting networkx>=2.0 (from openmdao)
Using cached networkx-3.3-py3-none-any.whl.metadata (5.1 kB)
Requirement already satisfied: numpy<2 in ./ESP_venv/lib/python3.11/site-packages (from openmdao) (1.26.4)
Collecting packaging (from openmdao)
Using cached packaging-24.0-py3-none-any.whl.metadata (3.2 kB)
Collecting requests (from openmdao)
Using cached requests-2.32.3-py3-none-any.whl.metadata (4.6 kB)
Collecting scipy (from openmdao)
Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (60 kB)
Collecting charset-normalizer<4,>=2 (from requests->openmdao)
Using cached charset_normalizer-3.3.2-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (33 kB)
Collecting idna<4,>=2.5 (from requests->openmdao)
Using cached idna-3.7-py3-none-any.whl.metadata (9.9 kB)
Collecting urllib3<3,>=1.21.1 (from requests->openmdao)
Using cached urllib3-2.2.1-py3-none-any.whl.metadata (6.4 kB)
Collecting certifi>=2017.4.17 (from requests->openmdao)
Using cached certifi-2024.2.2-py3-none-any.whl.metadata (2.2 kB)
Using cached networkx-3.3-py3-none-any.whl (1.7 MB)
Using cached packaging-24.0-py3-none-any.whl (53 kB)
Using cached requests-2.32.3-py3-none-any.whl (64 kB)
Using cached scipy-1.13.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (38.6 MB)
Using cached certifi-2024.2.2-py3-none-any.whl (163 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 urllib3-2.2.1-py3-none-any.whl (121 kB)
Installing collected packages: urllib3, scipy, packaging, networkx, idna, charset-normalizer, certifi, requests, openmdao
Successfully installed certifi-2024.2.2 charset-normalizer-3.3.2 idna-3.7 networkx-3.3 openmdao-3.32.0 packaging-24.0 requests-2.32.3 scipy-1.13.1 urllib3-2.2.1
+ [[ reynolds-centOS7 == *\v\i\g\g\e\n* ]]
+ pip_install cvxopt
+ /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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 (24.0)
+ pip_install matplotlib
+ /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin/python -m pip install --only-binary all --upgrade matplotlib
Collecting matplotlib
Using cached matplotlib-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (11 kB)
Collecting contourpy>=1.0.1 (from matplotlib)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (5.8 kB)
Collecting cycler>=0.10 (from matplotlib)
Using cached cycler-0.12.1-py3-none-any.whl.metadata (3.8 kB)
Collecting fonttools>=4.22.0 (from matplotlib)
Using cached fonttools-4.52.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl.metadata (161 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) (24.0)
Collecting pillow>=8 (from matplotlib)
Using cached pillow-10.3.0-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-3.9.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (8.3 MB)
Using cached contourpy-1.2.1-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (306 kB)
Using cached cycler-0.12.1-py3-none-any.whl (8.3 kB)
Using cached fonttools-4.52.4-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.9 MB)
Using cached kiwisolver-1.4.5-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (1.4 MB)
Using cached pillow-10.3.0-cp311-cp311-manylinux_2_17_x86_64.manylinux2014_x86_64.whl (4.4 MB)
Using cached pyparsing-3.1.2-py3-none-any.whl (103 kB)
Using cached python_dateutil-2.9.0.post0-py2.py3-none-any.whl (229 kB)
Using cached six-1.16.0-py2.py3-none-any.whl (11 kB)
Installing collected packages: six, pyparsing, pillow, kiwisolver, fonttools, cycler, contourpy, python-dateutil, matplotlib
Successfully installed contourpy-1.2.1 cycler-0.12.1 fonttools-4.52.4 kiwisolver-1.4.5 matplotlib-3.9.0 pillow-10.3.0 pyparsing-3.1.2 python-dateutil-2.9.0.post0 six-1.16.0
+ pip_install scipy
+ /home/jenkins/workspace/ESP_Beta/7.8/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 (1.13.1)
Requirement already satisfied: numpy<2.3,>=1.22.4 in ./ESP_venv/lib/python3.11/site-packages (from scipy) (1.26.4)
+ unset PYTHONINC
+ unset PYTHONLIB
+ unset UDUNITS2_XML_PATH
+ unset ESP_BLOC
+ unset ESP_ROOT
+ unset ESP_ARCH
+ unset AWAVE
+ unset AFLR
+ unset AFLR_ARCH
+ wget --tries=3 https://acdl.mit.edu/ESP/archive/ESPbeta.tgz
--2024-05-30 12:18:49-- 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: 272121672 (260M) [application/x-gzip]
Saving to: ‘ESPbeta.tgz’
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1850K .......... .......... .......... .......... .......... 0% 135M 8s
1900K .......... .......... .......... .......... .......... 0% 31.6M 8s
1950K .......... .......... .......... .......... .......... 0% 37.2M 8s
2000K .......... .......... .......... .......... .......... 0% 239M 7s
2050K .......... .......... .......... .......... .......... 0% 34.6M 7s
2100K .......... .......... .......... .......... .......... 0% 30.9M 7s
2150K .......... .......... .......... .......... .......... 0% 50.6M 7s
2200K .......... .......... .......... .......... .......... 0% 85.6M 7s
2250K .......... .......... .......... .......... .......... 0% 40.1M 7s
2300K .......... .......... .......... .......... .......... 0% 121M 7s
2350K .......... .......... .......... .......... .......... 0% 44.6M 7s
2400K .......... .......... .......... .......... .......... 0% 48.2M 7s
2450K .......... .......... .......... .......... .......... 0% 59.6M 7s
2500K .......... .......... .......... .......... .......... 0% 60.0M 7s
2550K .......... .......... .......... .......... .......... 0% 24.2M 7s
2600K .......... .......... .......... .......... .......... 0% 85.8M 7s
2650K .......... .......... .......... .......... .......... 1% 34.2M 7s
2700K .......... .......... .......... .......... .......... 1% 37.1M 7s
2750K .......... .......... .......... .......... .......... 1% 229M 7s
2800K .......... .......... .......... .......... .......... 1% 35.2M 7s
2850K .......... .......... .......... .......... .......... 1% 98.1M 7s
2900K .......... .......... .......... .......... .......... 1% 79.7M 7s
2950K .......... .......... .......... .......... .......... 1% 127M 7s
3000K .......... .......... .......... .......... .......... 1% 51.0M 7s
3050K .......... .......... .......... .......... .......... 1% 67.6M 7s
3100K .......... .......... .......... .......... .......... 1% 23.0M 7s
3150K .......... .......... .......... .......... .......... 1% 83.3M 7s
3200K .......... .......... .......... .......... .......... 1% 44.7M 7s
3250K .......... .......... .......... .......... .......... 1% 34.0M 7s
3300K .......... .......... .......... .......... .......... 1% 84.6M 7s
3350K .......... .......... .......... .......... .......... 1% 95.5M 6s
3400K .......... .......... .......... .......... .......... 1% 56.9M 6s
3450K .......... .......... .......... .......... .......... 1% 52.2M 6s
3500K .......... .......... .......... .......... .......... 1% 40.2M 6s
3550K .......... .......... .......... .......... .......... 1% 79.8M 6s
3600K .......... .......... .......... .......... .......... 1% 46.2M 6s
3650K .......... .......... .......... .......... .......... 1% 89.6M 6s
3700K .......... .......... .......... .......... .......... 1% 28.8M 6s
3750K .......... .......... .......... .......... .......... 1% 73.3M 6s
3800K .......... .......... .......... .......... .......... 1% 51.3M 6s
3850K .......... .......... .......... .......... .......... 1% 50.9M 6s
3900K .......... .......... .......... .......... .......... 1% 51.9M 6s
3950K .......... .......... .......... .......... .......... 1% 57.3M 6s
4000K .......... .......... .......... .......... .......... 1% 42.9M 6s
4050K .......... .......... .......... .......... .......... 1% 67.0M 6s
4100K .......... .......... .......... .......... .......... 1% 43.5M 6s
4150K .......... .......... .......... .......... .......... 1% 37.5M 6s
4200K .......... .......... .......... .......... .......... 1% 55.6M 6s
4250K .......... .......... .......... .......... .......... 1% 42.5M 6s
4300K .......... .......... .......... .......... .......... 1% 104M 6s
4350K .......... .......... .......... .......... .......... 1% 42.6M 6s
4400K .......... .......... .......... .......... .......... 1% 64.0M 6s
4450K .......... .......... .......... .......... .......... 1% 47.3M 6s
4500K .......... .......... .......... .......... .......... 1% 51.5M 6s
4550K .......... .......... .......... .......... .......... 1% 38.1M 6s
4600K .......... .......... .......... .......... .......... 1% 39.1M 6s
4650K .......... .......... .......... .......... .......... 1% 108M 6s
4700K .......... .......... .......... .......... .......... 1% 28.2M 6s
4750K .......... .......... .......... .......... .......... 1% 87.4M 6s
4800K .......... .......... .......... .......... .......... 1% 55.2M 6s
4850K .......... .......... .......... .......... .......... 1% 83.9M 6s
4900K .......... .......... .......... .......... .......... 1% 42.7M 6s
4950K .......... .......... .......... .......... .......... 1% 31.1M 6s
5000K .......... .......... .......... .......... .......... 1% 60.0M 6s
5050K .......... .......... .......... .......... .......... 1% 50.0M 6s
5100K .......... .......... .......... .......... .......... 1% 31.4M 6s
5150K .......... .......... .......... .......... .......... 1% 74.7M 6s
5200K .......... .......... .......... .......... .......... 1% 42.9M 6s
5250K .......... .......... .......... .......... .......... 1% 44.8M 6s
5300K .......... .......... .......... .......... .......... 2% 291M 6s
5350K .......... .......... .......... .......... .......... 2% 27.1M 6s
5400K .......... .......... .......... .......... .......... 2% 116M 6s
5450K .......... .......... .......... .......... .......... 2% 62.0M 6s
5500K .......... .......... .......... .......... .......... 2% 61.1M 6s
5550K .......... .......... .......... .......... .......... 2% 50.2M 6s
5600K .......... .......... .......... .......... .......... 2% 53.7M 6s
5650K .......... .......... .......... .......... .......... 2% 45.2M 6s
5700K .......... .......... .......... .......... .......... 2% 32.5M 6s
5750K .......... .......... .......... .......... .......... 2% 93.4M 6s
5800K .......... .......... .......... .......... .......... 2% 43.1M 6s
5850K .......... .......... .......... .......... .......... 2% 47.6M 6s
5900K .......... .......... .......... .......... .......... 2% 41.5M 6s
5950K .......... .......... .......... .......... .......... 2% 25.8M 6s
6000K .......... .......... .......... .......... .......... 2% 76.2M 6s
6050K .......... .......... .......... .......... .......... 2% 72.4M 6s
6100K .......... .......... .......... .......... .......... 2% 78.2M 6s
6150K .......... .......... .......... .......... .......... 2% 88.7M 6s
6200K .......... .......... .......... .......... .......... 2% 69.9M 6s
6250K .......... .......... .......... .......... .......... 2% 66.3M 6s
6300K .......... .......... .......... .......... .......... 2% 33.7M 6s
6350K .......... .......... .......... .......... .......... 2% 54.7M 6s
6400K .......... .......... .......... .......... .......... 2% 43.2M 6s
6450K .......... .......... .......... .......... .......... 2% 157M 6s
6500K .......... .......... .......... .......... .......... 2% 5.71M 6s
6550K .......... .......... .......... .......... .......... 2% 91.6M 6s
6600K .......... .......... .......... .......... .......... 2% 42.0M 6s
6650K .......... .......... .......... .......... .......... 2% 68.6M 6s
6700K .......... .......... .......... .......... .......... 2% 65.4M 6s
6750K .......... .......... .......... .......... .......... 2% 58.6M 6s
6800K .......... .......... .......... .......... .......... 2% 75.1M 6s
6850K .......... .......... .......... .......... .......... 2% 54.9M 6s
6900K .......... .......... .......... .......... .......... 2% 64.9M 6s
6950K .......... .......... .......... .......... .......... 2% 101M 6s
7000K .......... .......... .......... .......... .......... 2% 158M 6s
7050K .......... .......... .......... .......... .......... 2% 128M 6s
7100K .......... .......... .......... .......... .......... 2% 87.6M 6s
7150K .......... .......... .......... .......... .......... 2% 142M 6s
7200K .......... .......... .......... .......... .......... 2% 122M 6s
7250K .......... .......... .......... .......... .......... 2% 96.9M 6s
7300K .......... .......... .......... .......... .......... 2% 182M 6s
7350K .......... .......... .......... .......... .......... 2% 102M 6s
7400K .......... .......... .......... .......... .......... 2% 166M 6s
7450K .......... .......... .......... .......... .......... 2% 174M 6s
7500K .......... .......... .......... .......... .......... 2% 102M 6s
7550K .......... .......... .......... .......... .......... 2% 118M 6s
7600K .......... .......... .......... .......... .......... 2% 124M 6s
7650K .......... .......... .......... .......... .......... 2% 160M 5s
7700K .......... .......... .......... .......... .......... 2% 3.41M 6s
7750K .......... .......... .......... .......... .......... 2% 62.6M 6s
7800K .......... .......... .......... .......... .......... 2% 45.8M 6s
7850K .......... .......... .......... .......... .......... 2% 56.0M 6s
7900K .......... .......... .......... .......... .......... 2% 62.5M 6s
7950K .......... .......... .......... .......... .......... 3% 44.5M 6s
8000K .......... .......... .......... .......... .......... 3% 56.9M 6s
8050K .......... .......... .......... .......... .......... 3% 77.9M 6s
8100K .......... .......... .......... .......... .......... 3% 38.8M 6s
8150K .......... .......... .......... .......... .......... 3% 86.8M 6s
8200K .......... .......... .......... .......... .......... 3% 101M 6s
8250K .......... .......... .......... .......... .......... 3% 99.1M 6s
8300K .......... .......... .......... .......... .......... 3% 36.5M 6s
8350K .......... .......... .......... .......... .......... 3% 47.2M 6s
8400K .......... .......... .......... .......... .......... 3% 100M 6s
8450K .......... .......... .......... .......... .......... 3% 47.3M 6s
8500K .......... .......... .......... .......... .......... 3% 88.7M 6s
8550K .......... .......... .......... .......... .......... 3% 77.5M 6s
8600K .......... .......... .......... .......... .......... 3% 98.3M 6s
8650K .......... .......... .......... .......... .......... 3% 101M 6s
8700K .......... .......... .......... .......... .......... 3% 45.1M 6s
8750K .......... .......... .......... .......... .......... 3% 74.2M 6s
8800K .......... .......... .......... .......... .......... 3% 61.6M 6s
8850K .......... .......... .......... .......... .......... 3% 136M 6s
8900K .......... .......... .......... .......... .......... 3% 67.2M 6s
8950K .......... .......... .......... .......... .......... 3% 67.6M 6s
9000K .......... .......... .......... .......... .......... 3% 98.0M 6s
9050K .......... .......... .......... .......... .......... 3% 66.0M 6s
9100K .......... .......... .......... .......... .......... 3% 42.1M 6s
9150K .......... .......... .......... .......... .......... 3% 126M 6s
9200K .......... .......... .......... .......... .......... 3% 75.1M 6s
9250K .......... .......... .......... .......... .......... 3% 114M 6s
9300K .......... .......... .......... .......... .......... 3% 138M 6s
9350K .......... .......... .......... .......... .......... 3% 128M 6s
9400K .......... .......... .......... .......... .......... 3% 108M 5s
9450K .......... .......... .......... .......... .......... 3% 70.8M 5s
9500K .......... .......... .......... .......... .......... 3% 76.0M 5s
9550K .......... .......... .......... .......... .......... 3% 90.2M 5s
9600K .......... .......... .......... .......... .......... 3% 123M 5s
9650K .......... .......... .......... .......... .......... 3% 43.7M 5s
9700K .......... .......... .......... .......... .......... 3% 26.3M 5s
9750K .......... .......... .......... .......... .......... 3% 63.0M 5s
9800K .......... .......... .......... .......... .......... 3% 97.9M 5s
9850K .......... .......... .......... .......... .......... 3% 30.1M 5s
9900K .......... .......... .......... .......... .......... 3% 32.3M 5s
9950K .......... .......... .......... .......... .......... 3% 44.9M 5s
10000K .......... .......... .......... .......... .......... 3% 48.5M 5s
10050K .......... .......... .......... .......... .......... 3% 179M 5s
10100K .......... .......... .......... .......... .......... 3% 22.5M 5s
10150K .......... .......... .......... .......... .......... 3% 47.4M 5s
10200K .......... .......... .......... .......... .......... 3% 44.3M 5s
10250K .......... .......... .......... .......... .......... 3% 28.2M 5s
10300K .......... .......... .......... .......... .......... 3% 67.3M 5s
10350K .......... .......... .......... .......... .......... 3% 48.3M 5s
10400K .......... .......... .......... .......... .......... 3% 52.0M 5s
10450K .......... .......... .......... .......... .......... 3% 26.4M 5s
10500K .......... .......... .......... .......... .......... 3% 41.1M 5s
10550K .......... .......... .......... .......... .......... 3% 90.1M 5s
10600K .......... .......... .......... .......... .......... 4% 7.18M 6s
10650K .......... .......... .......... .......... .......... 4% 44.5M 6s
10700K .......... .......... .......... .......... .......... 4% 26.4M 6s
10750K .......... .......... .......... .......... .......... 4% 99.2M 6s
10800K .......... .......... .......... .......... .......... 4% 98.7M 6s
10850K .......... .......... .......... .......... .......... 4% 84.5M 6s
10900K .......... .......... .......... .......... .......... 4% 68.1M 6s
10950K .......... .......... .......... .......... .......... 4% 57.6M 6s
11000K .......... .......... .......... .......... .......... 4% 88.7M 6s
11050K .......... .......... .......... .......... .......... 4% 92.8M 6s
11100K .......... .......... .......... .......... .......... 4% 35.5M 6s
11150K .......... .......... .......... .......... .......... 4% 35.2M 6s
11200K .......... .......... .......... .......... .......... 4% 20.8M 6s
11250K .......... .......... .......... .......... .......... 4% 55.4M 6s
11300K .......... .......... .......... .......... .......... 4% 59.3M 6s
11350K .......... .......... .......... .......... .......... 4% 6.70M 6s
11400K .......... .......... .......... .......... .......... 4% 50.1M 6s
11450K .......... .......... .......... .......... .......... 4% 198M 6s
11500K .......... .......... .......... .......... .......... 4% 147M 6s
11550K .......... .......... .......... .......... .......... 4% 76.1M 6s
11600K .......... .......... .......... .......... .......... 4% 36.6M 6s
11650K .......... .......... .......... .......... .......... 4% 28.1M 6s
11700K .......... .......... .......... .......... .......... 4% 23.0M 6s
11750K .......... .......... .......... .......... .......... 4% 34.7M 6s
11800K .......... .......... .......... .......... .......... 4% 25.7M 6s
11850K .......... .......... .......... .......... .......... 4% 39.4M 6s
11900K .......... .......... .......... .......... .......... 4% 19.8M 6s
11950K .......... .......... .......... .......... .......... 4% 20.3M 6s
12000K .......... .......... .......... .......... .......... 4% 39.8M 6s
12050K .......... .......... .......... .......... .......... 4% 22.2M 6s
12100K .......... .......... .......... .......... .......... 4% 35.1M 6s
12150K .......... .......... .......... .......... .......... 4% 22.6M 6s
12200K .......... .......... .......... .......... .......... 4% 38.7M 6s
12250K .......... .......... .......... .......... .......... 4% 20.6M 6s
12300K .......... .......... .......... .......... .......... 4% 81.0M 6s
12350K .......... .......... .......... .......... .......... 4% 17.5M 6s
12400K .......... .......... .......... .......... .......... 4% 114M 6s
12450K .......... .......... .......... .......... .......... 4% 17.5M 6s
12500K .......... .......... .......... .......... .......... 4% 45.1M 6s
12550K .......... .......... .......... .......... .......... 4% 24.2M 6s
12600K .......... .......... .......... .......... .......... 4% 30.5M 6s
12650K .......... .......... .......... .......... .......... 4% 33.4M 6s
12700K .......... .......... .......... .......... .......... 4% 31.7M 6s
12750K .......... .......... .......... .......... .......... 4% 20.7M 6s
12800K .......... .......... .......... .......... .......... 4% 34.1M 6s
12850K .......... .......... .......... .......... .......... 4% 22.0M 6s
12900K .......... .......... .......... .......... .......... 4% 27.8M 6s
12950K .......... .......... .......... .......... .......... 4% 26.1M 6s
13000K .......... .......... .......... .......... .......... 4% 27.6M 6s
13050K .......... .......... .......... .......... .......... 4% 25.8M 6s
13100K .......... .......... .......... .......... .......... 4% 16.6M 6s
13150K .......... .......... .......... .......... .......... 4% 87.9M 6s
13200K .......... .......... .......... .......... .......... 4% 15.8M 6s
13250K .......... .......... .......... .......... .......... 5% 80.0M 6s
13300K .......... .......... .......... .......... .......... 5% 7.60M 6s
13350K .......... .......... .......... .......... .......... 5% 34.8M 6s
13400K .......... .......... .......... .......... .......... 5% 63.4M 6s
13450K .......... .......... .......... .......... .......... 5% 118M 6s
13500K .......... .......... .......... .......... .......... 5% 24.1M 6s
13550K .......... .......... .......... .......... .......... 5% 13.8M 6s
13600K .......... .......... .......... .......... .......... 5% 14.5M 6s
13650K .......... .......... .......... .......... .......... 5% 9.64M 6s
13700K .......... .......... .......... .......... .......... 5% 51.6M 6s
13750K .......... .......... .......... .......... .......... 5% 28.6M 6s
13800K .......... .......... .......... .......... .......... 5% 13.7M 6s
13850K .......... .......... .......... .......... .......... 5% 14.0M 6s
13900K .......... .......... .......... .......... .......... 5% 13.5M 6s
13950K .......... .......... .......... .......... .......... 5% 13.2M 6s
14000K .......... .......... .......... .......... .......... 5% 13.1M 6s
14050K .......... .......... .......... .......... .......... 5% 17.1M 6s
14100K .......... .......... .......... .......... .......... 5% 16.6M 7s
14150K .......... .......... .......... .......... .......... 5% 14.4M 7s
14200K .......... .......... .......... .......... .......... 5% 13.8M 7s
14250K .......... .......... .......... .......... .......... 5% 10.8M 7s
14300K .......... .......... .......... .......... .......... 5% 40.8M 7s
14350K .......... .......... .......... .......... .......... 5% 10.5M 7s
14400K .......... .......... .......... .......... .......... 5% 18.6M 7s
14450K .......... .......... .......... .......... .......... 5% 11.5M 7s
14500K .......... .......... .......... .......... .......... 5% 16.2M 7s
14550K .......... .......... .......... .......... .......... 5% 17.0M 7s
14600K .......... .......... .......... .......... .......... 5% 11.8M 7s
14650K .......... .......... .......... .......... .......... 5% 19.2M 7s
14700K .......... .......... .......... .......... .......... 5% 9.87M 7s
14750K .......... .......... .......... .......... .......... 5% 16.2M 7s
14800K .......... .......... .......... .......... .......... 5% 14.6M 7s
14850K .......... .......... .......... .......... .......... 5% 13.1M 7s
14900K .......... .......... .......... .......... .......... 5% 13.5M 7s
14950K .......... .......... .......... .......... .......... 5% 14.0M 7s
15000K .......... .......... .......... .......... .......... 5% 16.9M 7s
15050K .......... .......... .......... .......... .......... 5% 10.1M 7s
15100K .......... .......... .......... .......... .......... 5% 12.5M 7s
15150K .......... .......... .......... .......... .......... 5% 19.9M 7s
15200K .......... .......... .......... .......... .......... 5% 11.5M 7s
15250K .......... .......... .......... .......... .......... 5% 14.2M 7s
15300K .......... .......... .......... .......... .......... 5% 13.6M 7s
15350K .......... .......... .......... .......... .......... 5% 12.9M 7s
15400K .......... .......... .......... .......... .......... 5% 14.0M 7s
15450K .......... .......... .......... .......... .......... 5% 13.5M 7s
15500K .......... .......... .......... .......... .......... 5% 13.2M 7s
15550K .......... .......... .......... .......... .......... 5% 14.2M 8s
15600K .......... .......... .......... .......... .......... 5% 13.1M 8s
15650K .......... .......... .......... .......... .......... 5% 15.6M 8s
15700K .......... .......... .......... .......... .......... 5% 9.63M 8s
15750K .......... .......... .......... .......... .......... 5% 21.2M 8s
15800K .......... .......... .......... .......... .......... 5% 13.8M 8s
15850K .......... .......... .......... .......... .......... 5% 10.3M 8s
15900K .......... .......... .......... .......... .......... 6% 14.8M 8s
15950K .......... .......... .......... .......... .......... 6% 13.6M 8s
16000K .......... .......... .......... .......... .......... 6% 22.7M 8s
16050K .......... .......... .......... .......... .......... 6% 16.1M 8s
16100K .......... .......... .......... .......... .......... 6% 14.1M 8s
16150K .......... .......... .......... .......... .......... 6% 11.2M 8s
16200K .......... .......... .......... .......... .......... 6% 40.3M 8s
16250K .......... .......... .......... .......... .......... 6% 11.6M 8s
16300K .......... .......... .......... .......... .......... 6% 13.6M 8s
16350K .......... .......... .......... .......... .......... 6% 13.0M 8s
16400K .......... .......... .......... .......... .......... 6% 14.3M 8s
16450K .......... .......... .......... .......... .......... 6% 12.1M 8s
16500K .......... .......... .......... .......... .......... 6% 59.2M 8s
16550K .......... .......... .......... .......... .......... 6% 13.1M 8s
16600K .......... .......... .......... .......... .......... 6% 13.4M 8s
16650K .......... .......... .......... .......... .......... 6% 12.8M 8s
16700K .......... .......... .......... .......... .......... 6% 21.5M 8s
16750K .......... .......... .......... .......... .......... 6% 7.05M 8s
16800K .......... .......... .......... .......... .......... 6% 104M 8s
16850K .......... .......... .......... .......... .......... 6% 68.9M 8s
16900K .......... .......... .......... .......... .......... 6% 13.9M 8s
16950K .......... .......... .......... .......... .......... 6% 13.6M 8s
17000K .......... .......... .......... .......... .......... 6% 13.6M 8s
17050K .......... .......... .......... .......... .......... 6% 12.6M 8s
17100K .......... .......... .......... .......... .......... 6% 8.40M 8s
17150K .......... .......... .......... .......... .......... 6% 25.1M 8s
17200K .......... .......... .......... .......... .......... 6% 12.1M 8s
17250K .......... .......... .......... .......... .......... 6% 9.12M 8s
17300K .......... .......... .......... .......... .......... 6% 13.2M 8s
17350K .......... .......... .......... .......... .......... 6% 13.9M 8s
17400K .......... .......... .......... .......... .......... 6% 8.21M 9s
17450K .......... .......... .......... .......... .......... 6% 9.70M 9s
17500K .......... .......... .......... .......... .......... 6% 8.72M 9s
17550K .......... .......... .......... .......... .......... 6% 13.1M 9s
17600K .......... .......... .......... .......... .......... 6% 9.93M 9s
17650K .......... .......... .......... .......... .......... 6% 9.10M 9s
17700K .......... .......... .......... .......... .......... 6% 12.4M 9s
17750K .......... .......... .......... .......... .......... 6% 11.4M 9s
17800K .......... .......... .......... .......... .......... 6% 13.3M 9s
17850K .......... .......... .......... .......... .......... 6% 9.77M 9s
17900K .......... .......... .......... .......... .......... 6% 11.3M 9s
17950K .......... .......... .......... .......... .......... 6% 11.1M 9s
18000K .......... .......... .......... .......... .......... 6% 10.7M 9s
18050K .......... .......... .......... .......... .......... 6% 20.5M 9s
18100K .......... .......... .......... .......... .......... 6% 10.4M 9s
18150K .......... .......... .......... .......... .......... 6% 12.0M 9s
18200K .......... .......... .......... .......... .......... 6% 8.79M 9s
18250K .......... .......... .......... .......... .......... 6% 14.7M 9s
18300K .......... .......... .......... .......... .......... 6% 23.5M 9s
18350K .......... .......... .......... .......... .......... 6% 7.60M 9s
18400K .......... .......... .......... .......... .......... 6% 13.9M 9s
18450K .......... .......... .......... .......... .......... 6% 12.6M 9s
18500K .......... .......... .......... .......... .......... 6% 12.0M 9s
18550K .......... .......... .......... .......... .......... 6% 15.2M 9s
18600K .......... .......... .......... .......... .......... 7% 11.2M 9s
18650K .......... .......... .......... .......... .......... 7% 12.8M 9s
18700K .......... .......... .......... .......... .......... 7% 10.3M 9s
18750K .......... .......... .......... .......... .......... 7% 19.8M 9s
18800K .......... .......... .......... .......... .......... 7% 12.7M 9s
18850K .......... .......... .......... .......... .......... 7% 11.2M 9s
18900K .......... .......... .......... .......... .......... 7% 15.2M 9s
18950K .......... .......... .......... .......... .......... 7% 8.92M 9s
19000K .......... .......... .......... .......... .......... 7% 12.2M 9s
19050K .......... .......... .......... .......... .......... 7% 13.0M 10s
19100K .......... .......... .......... .......... .......... 7% 10.3M 10s
19150K .......... .......... .......... .......... .......... 7% 11.8M 10s
19200K .......... .......... .......... .......... .......... 7% 11.1M 10s
19250K .......... .......... .......... .......... .......... 7% 20.5M 10s
19300K .......... .......... .......... .......... .......... 7% 11.1M 10s
19350K .......... .......... .......... .......... .......... 7% 10.0M 10s
19400K .......... .......... .......... .......... .......... 7% 21.0M 10s
19450K .......... .......... .......... .......... .......... 7% 20.6M 10s
19500K .......... .......... .......... .......... .......... 7% 19.6M 10s
19550K .......... .......... .......... .......... .......... 7% 12.9M 10s
19600K .......... .......... .......... .......... .......... 7% 14.4M 10s
19650K .......... .......... .......... .......... .......... 7% 25.6M 10s
19700K .......... .......... .......... .......... .......... 7% 11.0M 10s
19750K .......... .......... .......... .......... .......... 7% 36.6M 10s
19800K .......... .......... .......... .......... .......... 7% 15.9M 10s
19850K .......... .......... .......... .......... .......... 7% 16.7M 10s
19900K .......... .......... .......... .......... .......... 7% 14.6M 10s
19950K .......... .......... .......... .......... .......... 7% 12.8M 10s
20000K .......... .......... .......... .......... .......... 7% 51.0M 10s
20050K .......... .......... .......... .......... .......... 7% 18.3M 10s
20100K .......... .......... .......... .......... .......... 7% 22.6M 10s
20150K .......... .......... .......... .......... .......... 7% 29.7M 10s
20200K .......... .......... .......... .......... .......... 7% 13.9M 10s
20250K .......... .......... .......... .......... .......... 7% 12.8M 10s
20300K .......... .......... .......... .......... .......... 7% 220M 10s
20350K .......... .......... .......... .......... .......... 7% 22.0M 10s
20400K .......... .......... .......... .......... .......... 7% 13.9M 10s
20450K .......... .......... .......... .......... .......... 7% 157M 10s
20500K .......... .......... .......... .......... .......... 7% 18.2M 10s
20550K .......... .......... .......... .......... .......... 7% 13.7M 10s
20600K .......... .......... .......... .......... .......... 7% 94.4M 10s
20650K .......... .......... .......... .......... .......... 7% 15.4M 10s
20700K .......... .......... .......... .......... .......... 7% 12.5M 10s
20750K .......... .......... .......... .......... .......... 7% 162M 10s
20800K .......... .......... .......... .......... .......... 7% 18.2M 10s
20850K .......... .......... .......... .......... .......... 7% 13.3M 10s
20900K .......... .......... .......... .......... .......... 7% 36.2M 10s
20950K .......... .......... .......... .......... .......... 7% 18.0M 10s
21000K .......... .......... .......... .......... .......... 7% 23.8M 10s
21050K .......... .......... .......... .......... .......... 7% 19.1M 10s
21100K .......... .......... .......... .......... .......... 7% 14.4M 10s
21150K .......... .......... .......... .......... .......... 7% 31.3M 10s
21200K .......... .......... .......... .......... .......... 7% 25.8M 10s
21250K .......... .......... .......... .......... .......... 8% 12.5M 10s
21300K .......... .......... .......... .......... .......... 8% 66.5M 10s
21350K .......... .......... .......... .......... .......... 8% 18.0M 10s
21400K .......... .......... .......... .......... .......... 8% 29.2M 10s
21450K .......... .......... .......... .......... .......... 8% 14.9M 10s
21500K .......... .......... .......... .......... .......... 8% 129M 10s
21550K .......... .......... .......... .......... .......... 8% 26.8M 10s
21600K .......... .......... .......... .......... .......... 8% 16.6M 10s
21650K .......... .......... .......... .......... .......... 8% 42.5M 10s
21700K .......... .......... .......... .......... .......... 8% 17.5M 10s
21750K .......... .......... .......... .......... .......... 8% 32.3M 10s
21800K .......... .......... .......... .......... .......... 8% 34.0M 10s
21850K .......... .......... .......... .......... .......... 8% 23.0M 10s
21900K .......... .......... .......... .......... .......... 8% 27.1M 10s
21950K .......... .......... .......... .......... .......... 8% 35.4M 10s
22000K .......... .......... .......... .......... .......... 8% 24.2M 10s
22050K .......... .......... .......... .......... .......... 8% 22.9M 10s
22100K .......... .......... .......... .......... .......... 8% 30.0M 10s
22150K .......... .......... .......... .......... .......... 8% 28.2M 10s
22200K .......... .......... .......... .......... .......... 8% 25.8M 10s
22250K .......... .......... .......... .......... .......... 8% 19.6M 10s
22300K .......... .......... .......... .......... .......... 8% 53.2M 10s
22350K .......... .......... .......... .......... .......... 8% 16.3M 10s
22400K .......... .......... .......... .......... .......... 8% 23.8M 10s
22450K .......... .......... .......... .......... .......... 8% 46.8M 10s
22500K .......... .......... .......... .......... .......... 8% 18.2M 10s
22550K .......... .......... .......... .......... .......... 8% 54.4M 10s
22600K .......... .......... .......... .......... .......... 8% 28.8M 10s
22650K .......... .......... .......... .......... .......... 8% 21.6M 10s
22700K .......... .......... .......... .......... .......... 8% 41.1M 10s
22750K .......... .......... .......... .......... .......... 8% 22.1M 10s
22800K .......... .......... .......... .......... .......... 8% 136M 10s
22850K .......... .......... .......... .......... .......... 8% 15.4M 10s
22900K .......... .......... .......... .......... .......... 8% 58.9M 10s
22950K .......... .......... .......... .......... .......... 8% 22.5M 10s
23000K .......... .......... .......... .......... .......... 8% 73.8M 10s
23050K .......... .......... .......... .......... .......... 8% 16.9M 10s
23100K .......... .......... .......... .......... .......... 8% 65.6M 10s
23150K .......... .......... .......... .......... .......... 8% 20.3M 10s
23200K .......... .......... .......... .......... .......... 8% 45.8M 10s
23250K .......... .......... .......... .......... .......... 8% 21.7M 10s
23300K .......... .......... .......... .......... .......... 8% 79.7M 10s
23350K .......... .......... .......... .......... .......... 8% 14.7M 10s
23400K .......... .......... .......... .......... .......... 8% 106M 10s
23450K .......... .......... .......... .......... .......... 8% 18.0M 10s
23500K .......... .......... .......... .......... .......... 8% 26.3M 10s
23550K .......... .......... .......... .......... .......... 8% 25.3M 10s
23600K .......... .......... .......... .......... .......... 8% 34.3M 10s
23650K .......... .......... .......... .......... .......... 8% 32.2M 10s
23700K .......... .......... .......... .......... .......... 8% 25.8M 10s
23750K .......... .......... .......... .......... .......... 8% 36.3M 10s
23800K .......... .......... .......... .......... .......... 8% 25.0M 10s
23850K .......... .......... .......... .......... .......... 8% 33.9M 10s
23900K .......... .......... .......... .......... .......... 9% 23.2M 10s
23950K .......... .......... .......... .......... .......... 9% 27.5M 10s
24000K .......... .......... .......... .......... .......... 9% 24.7M 10s
24050K .......... .......... .......... .......... .......... 9% 41.6M 10s
24100K .......... .......... .......... .......... .......... 9% 17.8M 10s
24150K .......... .......... .......... .......... .......... 9% 75.3M 10s
24200K .......... .......... .......... .......... .......... 9% 16.0M 10s
24250K .......... .......... .......... .......... .......... 9% 96.6M 10s
24300K .......... .......... .......... .......... .......... 9% 19.1M 10s
24350K .......... .......... .......... .......... .......... 9% 57.1M 10s
24400K .......... .......... .......... .......... .......... 9% 16.2M 10s
24450K .......... .......... .......... .......... .......... 9% 29.1M 10s
24500K .......... .......... .......... .......... .......... 9% 24.7M 10s
24550K .......... .......... .......... .......... .......... 9% 37.1M 10s
24600K .......... .......... .......... .......... .......... 9% 18.6M 10s
24650K .......... .......... .......... .......... .......... 9% 60.6M 10s
24700K .......... .......... .......... .......... .......... 9% 15.5M 10s
24750K .......... .......... .......... .......... .......... 9% 75.8M 10s
24800K .......... .......... .......... .......... .......... 9% 22.2M 10s
24850K .......... .......... .......... .......... .......... 9% 43.3M 10s
24900K .......... .......... .......... .......... .......... 9% 17.4M 10s
24950K .......... .......... .......... .......... .......... 9% 57.0M 10s
25000K .......... .......... .......... .......... .......... 9% 21.3M 10s
25050K .......... .......... .......... .......... .......... 9% 32.1M 10s
25100K .......... .......... .......... .......... .......... 9% 17.9M 10s
25150K .......... .......... .......... .......... .......... 9% 32.5M 10s
25200K .......... .......... .......... .......... .......... 9% 31.6M 10s
25250K .......... .......... .......... .......... .......... 9% 27.3M 10s
25300K .......... .......... .......... .......... .......... 9% 26.8M 10s
25350K .......... .......... .......... .......... .......... 9% 18.1M 10s
25400K .......... .......... .......... .......... .......... 9% 29.9M 10s
25450K .......... .......... .......... .......... .......... 9% 25.8M 10s
25500K .......... .......... .......... .......... .......... 9% 25.2M 10s
25550K .......... .......... .......... .......... .......... 9% 35.1M 10s
25600K .......... .......... .......... .......... .......... 9% 19.8M 10s
25650K .......... .......... .......... .......... .......... 9% 37.0M 9s
25700K .......... .......... .......... .......... .......... 9% 21.0M 9s
25750K .......... .......... .......... .......... .......... 9% 56.3M 9s
25800K .......... .......... .......... .......... .......... 9% 15.1M 9s
25850K .......... .......... .......... .......... .......... 9% 27.0M 9s
25900K .......... .......... .......... .......... .......... 9% 50.3M 9s
25950K .......... .......... .......... .......... .......... 9% 18.9M 9s
26000K .......... .......... .......... .......... .......... 9% 39.8M 9s
26050K .......... .......... .......... .......... .......... 9% 19.4M 9s
26100K .......... .......... .......... .......... .......... 9% 19.8M 9s
26150K .......... .......... .......... .......... .......... 9% 32.8M 9s
26200K .......... .......... .......... .......... .......... 9% 19.1M 9s
26250K .......... .......... .......... .......... .......... 9% 24.8M 9s
26300K .......... .......... .......... .......... .......... 9% 44.8M 9s
26350K .......... .......... .......... .......... .......... 9% 17.5M 9s
26400K .......... .......... .......... .......... .......... 9% 6.96M 10s
26450K .......... .......... .......... .......... .......... 9% 148M 9s
26500K .......... .......... .......... .......... .......... 9% 143M 9s
26550K .......... .......... .......... .......... .......... 10% 115M 9s
26600K .......... .......... .......... .......... .......... 10% 20.7M 9s
26650K .......... .......... .......... .......... .......... 10% 22.4M 9s
26700K .......... .......... .......... .......... .......... 10% 27.3M 9s
26750K .......... .......... .......... .......... .......... 10% 21.9M 9s
26800K .......... .......... .......... .......... .......... 10% 21.3M 9s
26850K .......... .......... .......... .......... .......... 10% 20.3M 9s
26900K .......... .......... .......... .......... .......... 10% 12.7M 9s
26950K .......... .......... .......... .......... .......... 10% 102M 9s
27000K .......... .......... .......... .......... .......... 10% 263M 9s
27050K .......... .......... .......... .......... .......... 10% 30.6M 9s
27100K .......... .......... .......... .......... .......... 10% 16.0M 9s
27150K .......... .......... .......... .......... .......... 10% 16.4M 9s
27200K .......... .......... .......... .......... .......... 10% 17.2M 9s
27250K .......... .......... .......... .......... .......... 10% 16.6M 9s
27300K .......... .......... .......... .......... .......... 10% 77.4M 9s
27350K .......... .......... .......... .......... .......... 10% 69.1M 9s
27400K .......... .......... .......... .......... .......... 10% 37.3M 9s
27450K .......... .......... .......... .......... .......... 10% 26.7M 9s
27500K .......... .......... .......... .......... .......... 10% 16.4M 9s
27550K .......... .......... .......... .......... .......... 10% 18.7M 9s
27600K .......... .......... .......... .......... .......... 10% 15.3M 9s
27650K .......... .......... .......... .......... .......... 10% 26.7M 9s
27700K .......... .......... .......... .......... .......... 10% 14.5M 9s
27750K .......... .......... .......... .......... .......... 10% 16.7M 9s
27800K .......... .......... .......... .......... .......... 10% 22.6M 9s
27850K .......... .......... .......... .......... .......... 10% 17.8M 9s
27900K .......... .......... .......... .......... .......... 10% 21.4M 9s
27950K .......... .......... .......... .......... .......... 10% 17.7M 9s
28000K .......... .......... .......... .......... .......... 10% 19.6M 9s
28050K .......... .......... .......... .......... .......... 10% 21.5M 9s
28100K .......... .......... .......... .......... .......... 10% 18.2M 9s
28150K .......... .......... .......... .......... .......... 10% 19.2M 9s
28200K .......... .......... .......... .......... .......... 10% 18.3M 9s
28250K .......... .......... .......... .......... .......... 10% 25.5M 9s
28300K .......... .......... .......... .......... .......... 10% 20.4M 9s
28350K .......... .......... .......... .......... .......... 10% 18.4M 9s
28400K .......... .......... .......... .......... .......... 10% 17.3M 9s
28450K .......... .......... .......... .......... .......... 10% 13.8M 10s
28500K .......... .......... .......... .......... .......... 10% 30.3M 9s
28550K .......... .......... .......... .......... .......... 10% 16.4M 10s
28600K .......... .......... .......... .......... .......... 10% 15.1M 10s
28650K .......... .......... .......... .......... .......... 10% 20.3M 10s
28700K .......... .......... .......... .......... .......... 10% 16.0M 10s
28750K .......... .......... .......... .......... .......... 10% 24.7M 10s
28800K .......... .......... .......... .......... .......... 10% 15.1M 10s
28850K .......... .......... .......... .......... .......... 10% 16.1M 10s
28900K .......... .......... .......... .......... .......... 10% 23.0M 10s
28950K .......... .......... .......... .......... .......... 10% 13.3M 10s
29000K .......... .......... .......... .......... .......... 10% 38.1M 10s
29050K .......... .......... .......... .......... .......... 10% 28.4M 10s
29100K .......... .......... .......... .......... .......... 10% 14.8M 10s
29150K .......... .......... .......... .......... .......... 10% 20.6M 10s
29200K .......... .......... .......... .......... .......... 11% 16.5M 10s
29250K .......... .......... .......... .......... .......... 11% 30.2M 10s
29300K .......... .......... .......... .......... .......... 11% 10.6M 10s
29350K .......... .......... .......... .......... .......... 11% 45.4M 10s
29400K .......... .......... .......... .......... .......... 11% 18.7M 10s
29450K .......... .......... .......... .......... .......... 11% 16.2M 10s
29500K .......... .......... .......... .......... .......... 11% 29.8M 10s
29550K .......... .......... .......... .......... .......... 11% 10.3M 10s
29600K .......... .......... .......... .......... .......... 11% 14.7M 10s
29650K .......... .......... .......... .......... .......... 11% 14.3M 10s
29700K .......... .......... .......... .......... .......... 11% 23.7M 10s
29750K .......... .......... .......... .......... .......... 11% 17.0M 10s
29800K .......... .......... .......... .......... .......... 11% 14.8M 10s
29850K .......... .......... .......... .......... .......... 11% 15.2M 10s
29900K .......... .......... .......... .......... .......... 11% 18.0M 10s
29950K .......... .......... .......... .......... .......... 11% 15.5M 10s
30000K .......... .......... .......... .......... .......... 11% 21.6M 10s
30050K .......... .......... .......... .......... .......... 11% 24.1M 10s
30100K .......... .......... .......... .......... .......... 11% 16.1M 10s
30150K .......... .......... .......... .......... .......... 11% 16.2M 10s
30200K .......... .......... .......... .......... .......... 11% 17.2M 10s
30250K .......... .......... .......... .......... .......... 11% 15.9M 10s
30300K .......... .......... .......... .......... .......... 11% 26.8M 10s
30350K .......... .......... .......... .......... .......... 11% 14.8M 10s
30400K .......... .......... .......... .......... .......... 11% 15.5M 10s
30450K .......... .......... .......... .......... .......... 11% 14.1M 10s
30500K .......... .......... .......... .......... .......... 11% 18.0M 10s
30550K .......... .......... .......... .......... .......... 11% 46.6M 10s
30600K .......... .......... .......... .......... .......... 11% 15.5M 10s
30650K .......... .......... .......... .......... .......... 11% 15.9M 10s
30700K .......... .......... .......... .......... .......... 11% 18.9M 10s
30750K .......... .......... .......... .......... .......... 11% 36.1M 10s
30800K .......... .......... .......... .......... .......... 11% 15.7M 10s
30850K .......... .......... .......... .......... .......... 11% 16.5M 10s
30900K .......... .......... .......... .......... .......... 11% 21.6M 10s
30950K .......... .......... .......... .......... .......... 11% 20.2M 10s
31000K .......... .......... .......... .......... .......... 11% 26.3M 10s
31050K .......... .......... .......... .......... .......... 11% 15.6M 10s
31100K .......... .......... .......... .......... .......... 11% 22.0M 10s
31150K .......... .......... .......... .......... .......... 11% 24.4M 10s
31200K .......... .......... .......... .......... .......... 11% 18.4M 10s
31250K .......... .......... .......... .......... .......... 11% 19.0M 10s
31300K .......... .......... .......... .......... .......... 11% 16.3M 10s
31350K .......... .......... .......... .......... .......... 11% 52.6M 10s
31400K .......... .......... .......... .......... .......... 11% 18.2M 10s
31450K .......... .......... .......... .......... .......... 11% 19.7M 10s
31500K .......... .......... .......... .......... .......... 11% 24.7M 10s
31550K .......... .......... .......... .......... .......... 11% 21.1M 10s
31600K .......... .......... .......... .......... .......... 11% 27.2M 10s
31650K .......... .......... .......... .......... .......... 11% 30.4M 10s
31700K .......... .......... .......... .......... .......... 11% 18.6M 10s
31750K .......... .......... .......... .......... .......... 11% 18.3M 10s
31800K .......... .......... .......... .......... .......... 11% 86.9M 10s
31850K .......... .......... .......... .......... .......... 12% 14.4M 10s
31900K .......... .......... .......... .......... .......... 12% 172M 10s
31950K .......... .......... .......... .......... .......... 12% 22.6M 10s
32000K .......... .......... .......... .......... .......... 12% 19.1M 10s
32050K .......... .......... .......... .......... .......... 12% 101M 10s
32100K .......... .......... .......... .......... .......... 12% 17.0M 10s
32150K .......... .......... .......... .......... .......... 12% 22.0M 10s
32200K .......... .......... .......... .......... .......... 12% 18.5M 10s
32250K .......... .......... .......... .......... .......... 12% 18.3M 10s
32300K .......... .......... .......... .......... .......... 12% 53.4M 10s
32350K .......... .......... .......... .......... .......... 12% 17.0M 10s
32400K .......... .......... .......... .......... .......... 12% 111M 10s
32450K .......... .......... .......... .......... .......... 12% 15.5M 10s
32500K .......... .......... .......... .......... .......... 12% 18.2M 10s
32550K .......... .......... .......... .......... .......... 12% 97.5M 10s
32600K .......... .......... .......... .......... .......... 12% 16.6M 10s
32650K .......... .......... .......... .......... .......... 12% 23.3M 10s
32700K .......... .......... .......... .......... .......... 12% 16.9M 10s
32750K .......... .......... .......... .......... .......... 12% 31.5M 10s
32800K .......... .......... .......... .......... .......... 12% 27.0M 10s
32850K .......... .......... .......... .......... .......... 12% 15.4M 10s
32900K .......... .......... .......... .......... .......... 12% 35.4M 10s
32950K .......... .......... .......... .......... .......... 12% 15.8M 10s
33000K .......... .......... .......... .......... .......... 12% 29.2M 10s
33050K .......... .......... .......... .......... .......... 12% 17.4M 10s
33100K .......... .......... .......... .......... .......... 12% 15.2M 10s
33150K .......... .......... .......... .......... .......... 12% 30.2M 10s
33200K .......... .......... .......... .......... .......... 12% 26.3M 10s
33250K .......... .......... .......... .......... .......... 12% 27.0M 10s
33300K .......... .......... .......... .......... .......... 12% 32.1M 10s
33350K .......... .......... .......... .......... .......... 12% 20.6M 10s
33400K .......... .......... .......... .......... .......... 12% 48.8M 10s
33450K .......... .......... .......... .......... .......... 12% 15.9M 10s
33500K .......... .......... .......... .......... .......... 12% 89.3M 10s
33550K .......... .......... .......... .......... .......... 12% 14.6M 10s
33600K .......... .......... .......... .......... .......... 12% 71.3M 10s
33650K .......... .......... .......... .......... .......... 12% 17.8M 10s
33700K .......... .......... .......... .......... .......... 12% 71.8M 10s
33750K .......... .......... .......... .......... .......... 12% 17.0M 10s
33800K .......... .......... .......... .......... .......... 12% 57.1M 10s
33850K .......... .......... .......... .......... .......... 12% 15.5M 10s
33900K .......... .......... .......... .......... .......... 12% 20.7M 10s
33950K .......... .......... .......... .......... .......... 12% 33.8M 10s
34000K .......... .......... .......... .......... .......... 12% 29.6M 10s
34050K .......... .......... .......... .......... .......... 12% 25.0M 10s
34100K .......... .......... .......... .......... .......... 12% 18.4M 10s
34150K .......... .......... .......... .......... .......... 12% 55.1M 10s
34200K .......... .......... .......... .......... .......... 12% 17.4M 10s
34250K .......... .......... .......... .......... .......... 12% 63.4M 10s
34300K .......... .......... .......... .......... .......... 12% 16.9M 10s
34350K .......... .......... .......... .......... .......... 12% 31.0M 10s
34400K .......... .......... .......... .......... .......... 12% 21.5M 10s
34450K .......... .......... .......... .......... .......... 12% 34.4M 10s
34500K .......... .......... .......... .......... .......... 13% 15.0M 10s
34550K .......... .......... .......... .......... .......... 13% 52.8M 10s
34600K .......... .......... .......... .......... .......... 13% 16.7M 10s
34650K .......... .......... .......... .......... .......... 13% 110M 10s
34700K .......... .......... .......... .......... .......... 13% 14.6M 10s
34750K .......... .......... .......... .......... .......... 13% 77.0M 10s
34800K .......... .......... .......... .......... .......... 13% 16.1M 10s
34850K .......... .......... .......... .......... .......... 13% 34.7M 10s
34900K .......... .......... .......... .......... .......... 13% 21.5M 10s
34950K .......... .......... .......... .......... .......... 13% 25.7M 9s
35000K .......... .......... .......... .......... .......... 13% 24.1M 9s
35050K .......... .......... .......... .......... .......... 13% 27.0M 9s
35100K .......... .......... .......... .......... .......... 13% 20.3M 9s
35150K .......... .......... .......... .......... .......... 13% 34.0M 9s
35200K .......... .......... .......... .......... .......... 13% 21.4M 9s
35250K .......... .......... .......... .......... .......... 13% 23.9M 9s
35300K .......... .......... .......... .......... .......... 13% 24.6M 9s
35350K .......... .......... .......... .......... .......... 13% 25.0M 9s
35400K .......... .......... .......... .......... .......... 13% 20.1M 9s
35450K .......... .......... .......... .......... .......... 13% 13.5M 9s
35500K .......... .......... .......... .......... .......... 13% 233M 9s
35550K .......... .......... .......... .......... .......... 13% 12.7M 9s
35600K .......... .......... .......... .......... .......... 13% 81.1M 9s
35650K .......... .......... .......... .......... .......... 13% 15.9M 9s
35700K .......... .......... .......... .......... .......... 13% 26.5M 9s
35750K .......... .......... .......... .......... .......... 13% 17.5M 9s
35800K .......... .......... .......... .......... .......... 13% 128M 9s
35850K .......... .......... .......... .......... .......... 13% 12.8M 9s
35900K .......... .......... .......... .......... .......... 13% 36.0M 9s
35950K .......... .......... .......... .......... .......... 13% 17.9M 9s
36000K .......... .......... .......... .......... .......... 13% 28.9M 9s
36050K .......... .......... .......... .......... .......... 13% 17.7M 9s
36100K .......... .......... .......... .......... .......... 13% 19.3M 9s
36150K .......... .......... .......... .......... .......... 13% 15.1M 9s
36200K .......... .......... .......... .......... .......... 13% 16.0M 9s
36250K .......... .......... .......... .......... .......... 13% 22.3M 9s
36300K .......... .......... .......... .......... .......... 13% 16.6M 9s
36350K .......... .......... .......... .......... .......... 13% 16.0M 9s
36400K .......... .......... .......... .......... .......... 13% 27.6M 9s
36450K .......... .......... .......... .......... .......... 13% 17.5M 9s
36500K .......... .......... .......... .......... .......... 13% 17.6M 9s
36550K .......... .......... .......... .......... .......... 13% 15.7M 9s
36600K .......... .......... .......... .......... .......... 13% 24.3M 9s
36650K .......... .......... .......... .......... .......... 13% 13.1M 9s
36700K .......... .......... .......... .......... .......... 13% 24.2M 9s
36750K .......... .......... .......... .......... .......... 13% 15.5M 9s
36800K .......... .......... .......... .......... .......... 13% 28.6M 9s
36850K .......... .......... .......... .......... .......... 13% 16.6M 9s
36900K .......... .......... .......... .......... .......... 13% 27.8M 9s
36950K .......... .......... .......... .......... .......... 13% 12.6M 9s
37000K .......... .......... .......... .......... .......... 13% 30.4M 9s
37050K .......... .......... .......... .......... .......... 13% 13.5M 10s
37100K .......... .......... .......... .......... .......... 13% 17.3M 10s
37150K .......... .......... .......... .......... .......... 13% 16.2M 10s
37200K .......... .......... .......... .......... .......... 14% 26.1M 10s
37250K .......... .......... .......... .......... .......... 14% 19.1M 10s
37300K .......... .......... .......... .......... .......... 14% 24.3M 10s
37350K .......... .......... .......... .......... .......... 14% 19.8M 10s
37400K .......... .......... .......... .......... .......... 14% 17.9M 10s
37450K .......... .......... .......... .......... .......... 14% 26.4M 10s
37500K .......... .......... .......... .......... .......... 14% 30.2M 9s
37550K .......... .......... .......... .......... .......... 14% 18.1M 9s
37600K .......... .......... .......... .......... .......... 14% 27.8M 9s
37650K .......... .......... .......... .......... .......... 14% 19.3M 9s
37700K .......... .......... .......... .......... .......... 14% 19.8M 9s
37750K .......... .......... .......... .......... .......... 14% 17.8M 9s
37800K .......... .......... .......... .......... .......... 14% 64.4M 9s
37850K .......... .......... .......... .......... .......... 14% 16.7M 9s
37900K .......... .......... .......... .......... .......... 14% 40.4M 9s
37950K .......... .......... .......... .......... .......... 14% 24.5M 9s
38000K .......... .......... .......... .......... .......... 14% 26.4M 9s
38050K .......... .......... .......... .......... .......... 14% 11.9M 9s
38100K .......... .......... .......... .......... .......... 14% 77.1M 9s
38150K .......... .......... .......... .......... .......... 14% 18.0M 9s
38200K .......... .......... .......... .......... .......... 14% 71.2M 9s
38250K .......... .......... .......... .......... .......... 14% 12.7M 9s
38300K .......... .......... .......... .......... .......... 14% 28.0M 9s
38350K .......... .......... .......... .......... .......... 14% 59.5M 9s
38400K .......... .......... .......... .......... .......... 14% 21.7M 9s
38450K .......... .......... .......... .......... .......... 14% 52.4M 9s
38500K .......... .......... .......... .......... .......... 14% 20.7M 9s
38550K .......... .......... .......... .......... .......... 14% 23.3M 9s
38600K .......... .......... .......... .......... .......... 14% 21.7M 9s
38650K .......... .......... .......... .......... .......... 14% 30.9M 9s
38700K .......... .......... .......... .......... .......... 14% 91.2M 9s
38750K .......... .......... .......... .......... .......... 14% 14.2M 9s
38800K .......... .......... .......... .......... .......... 14% 36.0M 9s
38850K .......... .......... .......... .......... .......... 14% 27.1M 9s
38900K .......... .......... .......... .......... .......... 14% 23.7M 9s
38950K .......... .......... .......... .......... .......... 14% 28.5M 9s
39000K .......... .......... .......... .......... .......... 14% 16.1M 9s
39050K .......... .......... .......... .......... .......... 14% 19.1M 9s
39100K .......... .......... .......... .......... .......... 14% 50.1M 9s
39150K .......... .......... .......... .......... .......... 14% 18.7M 9s
39200K .......... .......... .......... .......... .......... 14% 37.9M 9s
39250K .......... .......... .......... .......... .......... 14% 17.6M 9s
39300K .......... .......... .......... .......... .......... 14% 42.3M 9s
39350K .......... .......... .......... .......... .......... 14% 16.5M 9s
39400K .......... .......... .......... .......... .......... 14% 27.6M 9s
39450K .......... .......... .......... .......... .......... 14% 23.2M 9s
39500K .......... .......... .......... .......... .......... 14% 16.2M 9s
39550K .......... .......... .......... .......... .......... 14% 6.32M 9s
39600K .......... .......... .......... .......... .......... 14% 215M 9s
39650K .......... .......... .......... .......... .......... 14% 30.1M 9s
39700K .......... .......... .......... .......... .......... 14% 224M 9s
39750K .......... .......... .......... .......... .......... 14% 155M 9s
39800K .......... .......... .......... .......... .......... 14% 16.3M 9s
39850K .......... .......... .......... .......... .......... 15% 28.1M 9s
39900K .......... .......... .......... .......... .......... 15% 12.6M 9s
39950K .......... .......... .......... .......... .......... 15% 24.2M 9s
40000K .......... .......... .......... .......... .......... 15% 18.5M 9s
40050K .......... .......... .......... .......... .......... 15% 16.0M 9s
40100K .......... .......... .......... .......... .......... 15% 19.7M 9s
40150K .......... .......... .......... .......... .......... 15% 12.7M 9s
40200K .......... .......... .......... .......... .......... 15% 60.7M 9s
40250K .......... .......... .......... .......... .......... 15% 21.2M 9s
40300K .......... .......... .......... .......... .......... 15% 27.1M 9s
40350K .......... .......... .......... .......... .......... 15% 15.4M 9s
40400K .......... .......... .......... .......... .......... 15% 21.3M 9s
40450K .......... .......... .......... .......... .......... 15% 19.1M 9s
40500K .......... .......... .......... .......... .......... 15% 21.3M 9s
40550K .......... .......... .......... .......... .......... 15% 29.1M 9s
40600K .......... .......... .......... .......... .......... 15% 12.6M 9s
40650K .......... .......... .......... .......... .......... 15% 37.8M 9s
40700K .......... .......... .......... .......... .......... 15% 17.1M 9s
40750K .......... .......... .......... .......... .......... 15% 25.6M 9s
40800K .......... .......... .......... .......... .......... 15% 25.8M 9s
40850K .......... .......... .......... .......... .......... 15% 18.7M 9s
40900K .......... .......... .......... .......... .......... 15% 21.4M 9s
40950K .......... .......... .......... .......... .......... 15% 29.4M 9s
41000K .......... .......... .......... .......... .......... 15% 13.5M 9s
41050K .......... .......... .......... .......... .......... 15% 79.4M 9s
41100K .......... .......... .......... .......... .......... 15% 14.3M 9s
41150K .......... .......... .......... .......... .......... 15% 62.2M 9s
41200K .......... .......... .......... .......... .......... 15% 12.5M 9s
41250K .......... .......... .......... .......... .......... 15% 35.7M 9s
41300K .......... .......... .......... .......... .......... 15% 18.8M 9s
41350K .......... .......... .......... .......... .......... 15% 30.5M 9s
41400K .......... .......... .......... .......... .......... 15% 20.5M 9s
41450K .......... .......... .......... .......... .......... 15% 22.2M 9s
41500K .......... .......... .......... .......... .......... 15% 23.9M 9s
41550K .......... .......... .......... .......... .......... 15% 22.0M 9s
41600K .......... .......... .......... .......... .......... 15% 21.1M 9s
41650K .......... .......... .......... .......... .......... 15% 16.3M 9s
41700K .......... .......... .......... .......... .......... 15% 56.2M 9s
41750K .......... .......... .......... .......... .......... 15% 14.2M 9s
41800K .......... .......... .......... .......... .......... 15% 60.6M 9s
41850K .......... .......... .......... .......... .......... 15% 12.6M 9s
41900K .......... .......... .......... .......... .......... 15% 59.2M 9s
41950K .......... .......... .......... .......... .......... 15% 13.6M 9s
42000K .......... .......... .......... .......... .......... 15% 31.8M 9s
42050K .......... .......... .......... .......... .......... 15% 17.1M 9s
42100K .......... .......... .......... .......... .......... 15% 14.8M 9s
42150K .......... .......... .......... .......... .......... 15% 36.5M 9s
42200K .......... .......... .......... .......... .......... 15% 17.8M 9s
42250K .......... .......... .......... .......... .......... 15% 31.4M 9s
42300K .......... .......... .......... .......... .......... 15% 17.3M 9s
42350K .......... .......... .......... .......... .......... 15% 94.6M 9s
42400K .......... .......... .......... .......... .......... 15% 12.5M 9s
42450K .......... .......... .......... .......... .......... 15% 46.3M 9s
42500K .......... .......... .......... .......... .......... 16% 13.0M 9s
42550K .......... .......... .......... .......... .......... 16% 27.4M 9s
42600K .......... .......... .......... .......... .......... 16% 38.0M 9s
42650K .......... .......... .......... .......... .......... 16% 13.6M 9s
42700K .......... .......... .......... .......... .......... 16% 42.3M 9s
42750K .......... .......... .......... .......... .......... 16% 13.4M 9s
42800K .......... .......... .......... .......... .......... 16% 44.6M 9s
42850K .......... .......... .......... .......... .......... 16% 15.9M 9s
42900K .......... .......... .......... .......... .......... 16% 16.0M 9s
42950K .......... .......... .......... .......... .......... 16% 22.3M 9s
43000K .......... .......... .......... .......... .......... 16% 53.8M 9s
43050K .......... .......... .......... .......... .......... 16% 13.5M 9s
43100K .......... .......... .......... .......... .......... 16% 32.5M 9s
43150K .......... .......... .......... .......... .......... 16% 16.2M 9s
43200K .......... .......... .......... .......... .......... 16% 27.1M 9s
43250K .......... .......... .......... .......... .......... 16% 13.9M 9s
43300K .......... .......... .......... .......... .......... 16% 35.3M 9s
43350K .......... .......... .......... .......... .......... 16% 16.9M 9s
43400K .......... .......... .......... .......... .......... 16% 27.2M 9s
43450K .......... .......... .......... .......... .......... 16% 20.0M 9s
43500K .......... .......... .......... .......... .......... 16% 17.5M 9s
43550K .......... .......... .......... .......... .......... 16% 39.2M 9s
43600K .......... .......... .......... .......... .......... 16% 14.0M 9s
43650K .......... .......... .......... .......... .......... 16% 36.1M 9s
43700K .......... .......... .......... .......... .......... 16% 13.1M 9s
43750K .......... .......... .......... .......... .......... 16% 35.9M 9s
43800K .......... .......... .......... .......... .......... 16% 17.7M 9s
43850K .......... .......... .......... .......... .......... 16% 24.3M 9s
43900K .......... .......... .......... .......... .......... 16% 35.3M 9s
43950K .......... .......... .......... .......... .......... 16% 17.0M 9s
44000K .......... .......... .......... .......... .......... 16% 26.4M 9s
44050K .......... .......... .......... .......... .......... 16% 14.0M 9s
44100K .......... .......... .......... .......... .......... 16% 59.3M 9s
44150K .......... .......... .......... .......... .......... 16% 21.1M 9s
44200K .......... .......... .......... .......... .......... 16% 22.0M 9s
44250K .......... .......... .......... .......... .......... 16% 19.1M 9s
44300K .......... .......... .......... .......... .......... 16% 25.0M 9s
44350K .......... .......... .......... .......... .......... 16% 26.9M 9s
44400K .......... .......... .......... .......... .......... 16% 16.1M 9s
44450K .......... .......... .......... .......... .......... 16% 31.1M 9s
44500K .......... .......... .......... .......... .......... 16% 16.2M 9s
44550K .......... .......... .......... .......... .......... 16% 34.4M 9s
44600K .......... .......... .......... .......... .......... 16% 27.2M 9s
44650K .......... .......... .......... .......... .......... 16% 19.1M 9s
44700K .......... .......... .......... .......... .......... 16% 15.7M 9s
44750K .......... .......... .......... .......... .......... 16% 20.6M 9s
44800K .......... .......... .......... .......... .......... 16% 158M 9s
44850K .......... .......... .......... .......... .......... 16% 17.7M 9s
44900K .......... .......... .......... .......... .......... 16% 23.0M 9s
44950K .......... .......... .......... .......... .......... 16% 18.0M 9s
45000K .......... .......... .......... .......... .......... 16% 25.8M 9s
45050K .......... .......... .......... .......... .......... 16% 48.8M 9s
45100K .......... .......... .......... .......... .......... 16% 17.9M 9s
45150K .......... .......... .......... .......... .......... 17% 33.4M 9s
45200K .......... .......... .......... .......... .......... 17% 14.8M 9s
45250K .......... .......... .......... .......... .......... 17% 30.6M 9s
45300K .......... .......... .......... .......... .......... 17% 47.4M 9s
45350K .......... .......... .......... .......... .......... 17% 22.1M 9s
45400K .......... .......... .......... .......... .......... 17% 26.7M 9s
45450K .......... .......... .......... .......... .......... 17% 15.3M 9s
45500K .......... .......... .......... .......... .......... 17% 38.7M 9s
45550K .......... .......... .......... .......... .......... 17% 46.7M 9s
45600K .......... .......... .......... .......... .......... 17% 19.3M 9s
45650K .......... .......... .......... .......... .......... 17% 24.5M 9s
45700K .......... .......... .......... .......... .......... 17% 16.6M 9s
45750K .......... .......... .......... .......... .......... 17% 114M 9s
45800K .......... .......... .......... .......... .......... 17% 23.8M 9s
45850K .......... .......... .......... .......... .......... 17% 18.7M 9s
45900K .......... .......... .......... .......... .......... 17% 20.0M 9s
45950K .......... .......... .......... .......... .......... 17% 23.1M 9s
46000K .......... .......... .......... .......... .......... 17% 121M 9s
46050K .......... .......... .......... .......... .......... 17% 17.7M 9s
46100K .......... .......... .......... .......... .......... 17% 23.3M 9s
46150K .......... .......... .......... .......... .......... 17% 18.5M 9s
46200K .......... .......... .......... .......... .......... 17% 23.4M 9s
46250K .......... .......... .......... .......... .......... 17% 66.2M 9s
46300K .......... .......... .......... .......... .......... 17% 14.1M 9s
46350K .......... .......... .......... .......... .......... 17% 22.3M 9s
46400K .......... .......... .......... .......... .......... 17% 15.8M 9s
46450K .......... .......... .......... .......... .......... 17% 26.9M 9s
46500K .......... .......... .......... .......... .......... 17% 72.8M 9s
46550K .......... .......... .......... .......... .......... 17% 17.6M 9s
46600K .......... .......... .......... .......... .......... 17% 20.4M 9s
46650K .......... .......... .......... .......... .......... 17% 17.4M 9s
46700K .......... .......... .......... .......... .......... 17% 33.2M 9s
46750K .......... .......... .......... .......... .......... 17% 62.6M 9s
46800K .......... .......... .......... .......... .......... 17% 14.8M 9s
46850K .......... .......... .......... .......... .......... 17% 26.8M 9s
46900K .......... .......... .......... .......... .......... 17% 16.1M 9s
46950K .......... .......... .......... .......... .......... 17% 67.4M 9s
47000K .......... .......... .......... .......... .......... 17% 24.2M 9s
47050K .......... .......... .......... .......... .......... 17% 16.1M 9s
47100K .......... .......... .......... .......... .......... 17% 23.8M 9s
47150K .......... .......... .......... .......... .......... 17% 16.2M 9s
47200K .......... .......... .......... .......... .......... 17% 51.0M 9s
47250K .......... .......... .......... .......... .......... 17% 22.8M 9s
47300K .......... .......... .......... .......... .......... 17% 18.6M 9s
47350K .......... .......... .......... .......... .......... 17% 23.4M 9s
47400K .......... .......... .......... .......... .......... 17% 50.8M 9s
47450K .......... .......... .......... .......... .......... 17% 15.7M 9s
47500K .......... .......... .......... .......... .......... 17% 23.6M 9s
47550K .......... .......... .......... .......... .......... 17% 20.9M 9s
47600K .......... .......... .......... .......... .......... 17% 19.2M 9s
47650K .......... .......... .......... .......... .......... 17% 53.7M 9s
47700K .......... .......... .......... .......... .......... 17% 16.0M 9s
47750K .......... .......... .......... .......... .......... 17% 24.1M 9s
47800K .......... .......... .......... .......... .......... 18% 35.4M 9s
47850K .......... .......... .......... .......... .......... 18% 11.5M 9s
47900K .......... .......... .......... .......... .......... 18% 31.8M 9s
47950K .......... .......... .......... .......... .......... 18% 20.6M 9s
48000K .......... .......... .......... .......... .......... 18% 21.9M 9s
48050K .......... .......... .......... .......... .......... 18% 55.0M 9s
48100K .......... .......... .......... .......... .......... 18% 12.0M 9s
48150K .......... .......... .......... .......... .......... 18% 28.4M 9s
48200K .......... .......... .......... .......... .......... 18% 28.1M 9s
48250K .......... .......... .......... .......... .......... 18% 17.4M 9s
48300K .......... .......... .......... .......... .......... 18% 37.1M 9s
48350K .......... .......... .......... .......... .......... 18% 14.1M 9s
48400K .......... .......... .......... .......... .......... 18% 38.0M 9s
48450K .......... .......... .......... .......... .......... 18% 20.1M 9s
48500K .......... .......... .......... .......... .......... 18% 23.0M 9s
48550K .......... .......... .......... .......... .......... 18% 30.1M 9s
48600K .......... .......... .......... .......... .......... 18% 25.2M 9s
48650K .......... .......... .......... .......... .......... 18% 17.6M 9s
48700K .......... .......... .......... .......... .......... 18% 21.3M 9s
48750K .......... .......... .......... .......... .......... 18% 38.5M 9s
48800K .......... .......... .......... .......... .......... 18% 16.4M 9s
48850K .......... .......... .......... .......... .......... 18% 30.3M 9s
48900K .......... .......... .......... .......... .......... 18% 15.7M 9s
48950K .......... .......... .......... .......... .......... 18% 18.7M 9s
49000K .......... .......... .......... .......... .......... 18% 36.3M 9s
49050K .......... .......... .......... .......... .......... 18% 30.7M 9s
49100K .......... .......... .......... .......... .......... 18% 16.5M 9s
49150K .......... .......... .......... .......... .......... 18% 20.5M 9s
49200K .......... .......... .......... .......... .......... 18% 9.12M 9s
49250K .......... .......... .......... .......... .......... 18% 23.3M 9s
49300K .......... .......... .......... .......... .......... 18% 9.50M 9s
49350K .......... .......... .......... .......... .......... 18% 54.5M 9s
49400K .......... .......... .......... .......... .......... 18% 96.8M 9s
49450K .......... .......... .......... .......... .......... 18% 11.1M 9s
49500K .......... .......... .......... .......... .......... 18% 150M 9s
49550K .......... .......... .......... .......... .......... 18% 18.4M 9s
49600K .......... .......... .......... .......... .......... 18% 45.7M 9s
49650K .......... .......... .......... .......... .......... 18% 57.6M 9s
49700K .......... .......... .......... .......... .......... 18% 17.2M 9s
49750K .......... .......... .......... .......... .......... 18% 80.0M 9s
49800K .......... .......... .......... .......... .......... 18% 40.2M 9s
49850K .......... .......... .......... .......... .......... 18% 18.8M 9s
49900K .......... .......... .......... .......... .......... 18% 40.9M 9s
49950K .......... .......... .......... .......... .......... 18% 29.6M 9s
50000K .......... .......... .......... .......... .......... 18% 77.7M 9s
50050K .......... .......... .......... .......... .......... 18% 38.8M 9s
50100K .......... .......... .......... .......... .......... 18% 37.9M 9s
50150K .......... .......... .......... .......... .......... 18% 96.8M 9s
50200K .......... .......... .......... .......... .......... 18% 27.0M 9s
50250K .......... .......... .......... .......... .......... 18% 45.0M 9s
50300K .......... .......... .......... .......... .......... 18% 30.0M 9s
50350K .......... .......... .......... .......... .......... 18% 24.5M 9s
50400K .......... .......... .......... .......... .......... 18% 60.8M 9s
50450K .......... .......... .......... .......... .......... 19% 18.6M 9s
50500K .......... .......... .......... .......... .......... 19% 130M 9s
50550K .......... .......... .......... .......... .......... 19% 54.2M 9s
50600K .......... .......... .......... .......... .......... 19% 23.9M 9s
50650K .......... .......... .......... .......... .......... 19% 19.9M 9s
50700K .......... .......... .......... .......... .......... 19% 21.9M 9s
50750K .......... .......... .......... .......... .......... 19% 39.7M 9s
50800K .......... .......... .......... .......... .......... 19% 39.0M 9s
50850K .......... .......... .......... .......... .......... 19% 17.5M 9s
50900K .......... .......... .......... .......... .......... 19% 22.6M 9s
50950K .......... .......... .......... .......... .......... 19% 14.3M 9s
51000K .......... .......... .......... .......... .......... 19% 15.0M 9s
51050K .......... .......... .......... .......... .......... 19% 39.4M 9s
51100K .......... .......... .......... .......... .......... 19% 15.2M 9s
51150K .......... .......... .......... .......... .......... 19% 16.6M 9s
51200K .......... .......... .......... .......... .......... 19% 14.5M 9s
51250K .......... .......... .......... .......... .......... 19% 50.9M 9s
51300K .......... .......... .......... .......... .......... 19% 13.7M 9s
51350K .......... .......... .......... .......... .......... 19% 11.8M 9s
51400K .......... .......... .......... .......... .......... 19% 13.3M 9s
51450K .......... .......... .......... .......... .......... 19% 28.7M 9s
51500K .......... .......... .......... .......... .......... 19% 11.3M 9s
51550K .......... .......... .......... .......... .......... 19% 14.1M 9s
51600K .......... .......... .......... .......... .......... 19% 17.7M 9s
51650K .......... .......... .......... .......... .......... 19% 15.7M 9s
51700K .......... .......... .......... .......... .......... 19% 14.1M 9s
51750K .......... .......... .......... .......... .......... 19% 23.4M 9s
51800K .......... .......... .......... .......... .......... 19% 126M 9s
51850K .......... .......... .......... .......... .......... 19% 19.6M 9s
51900K .......... .......... .......... .......... .......... 19% 21.1M 9s
51950K .......... .......... .......... .......... .......... 19% 12.9M 9s
52000K .......... .......... .......... .......... .......... 19% 38.5M 9s
52050K .......... .......... .......... .......... .......... 19% 16.9M 9s
52100K .......... .......... .......... .......... .......... 19% 14.3M 9s
52150K .......... .......... .......... .......... .......... 19% 19.3M 9s
52200K .......... .......... .......... .......... .......... 19% 47.0M 9s
52250K .......... .......... .......... .......... .......... 19% 16.1M 9s
52300K .......... .......... .......... .......... .......... 19% 22.6M 9s
52350K .......... .......... .......... .......... .......... 19% 18.1M 9s
52400K .......... .......... .......... .......... .......... 19% 17.3M 9s
52450K .......... .......... .......... .......... .......... 19% 15.8M 9s
52500K .......... .......... .......... .......... .......... 19% 31.7M 9s
52550K .......... .......... .......... .......... .......... 19% 13.0M 9s
52600K .......... .......... .......... .......... .......... 19% 16.2M 9s
52650K .......... .......... .......... .......... .......... 19% 15.3M 9s
52700K .......... .......... .......... .......... .......... 19% 42.7M 9s
52750K .......... .......... .......... .......... .......... 19% 70.2M 9s
52800K .......... .......... .......... .......... .......... 19% 18.9M 9s
52850K .......... .......... .......... .......... .......... 19% 48.8M 9s
52900K .......... .......... .......... .......... .......... 19% 26.4M 9s
52950K .......... .......... .......... .......... .......... 19% 23.0M 9s
53000K .......... .......... .......... .......... .......... 19% 17.8M 9s
53050K .......... .......... .......... .......... .......... 19% 18.7M 9s
53100K .......... .......... .......... .......... .......... 20% 15.1M 9s
53150K .......... .......... .......... .......... .......... 20% 21.3M 9s
53200K .......... .......... .......... .......... .......... 20% 34.8M 9s
53250K .......... .......... .......... .......... .......... 20% 20.4M 9s
53300K .......... .......... .......... .......... .......... 20% 20.8M 9s
53350K .......... .......... .......... .......... .......... 20% 18.1M 9s
53400K .......... .......... .......... .......... .......... 20% 24.0M 9s
53450K .......... .......... .......... .......... .......... 20% 52.3M 9s
53500K .......... .......... .......... .......... .......... 20% 23.9M 9s
53550K .......... .......... .......... .......... .......... 20% 27.0M 9s
53600K .......... .......... .......... .......... .......... 20% 14.1M 9s
53650K .......... .......... .......... .......... .......... 20% 124M 9s
53700K .......... .......... .......... .......... .......... 20% 24.1M 9s
53750K .......... .......... .......... .......... .......... 20% 15.4M 9s
53800K .......... .......... .......... .......... .......... 20% 23.1M 9s
53850K .......... .......... .......... .......... .......... 20% 16.4M 9s
53900K .......... .......... .......... .......... .......... 20% 30.7M 9s
53950K .......... .......... .......... .......... .......... 20% 17.9M 9s
54000K .......... .......... .......... .......... .......... 20% 21.0M 9s
54050K .......... .......... .......... .......... .......... 20% 19.8M 9s
54100K .......... .......... .......... .......... .......... 20% 15.6M 9s
54150K .......... .......... .......... .......... .......... 20% 48.3M 9s
54200K .......... .......... .......... .......... .......... 20% 15.5M 9s
54250K .......... .......... .......... .......... .......... 20% 25.4M 9s
54300K .......... .......... .......... .......... .......... 20% 19.9M 9s
54350K .......... .......... .......... .......... .......... 20% 14.0M 9s
54400K .......... .......... .......... .......... .......... 20% 46.0M 9s
54450K .......... .......... .......... .......... .......... 20% 26.5M 9s
54500K .......... .......... .......... .......... .......... 20% 22.4M 9s
54550K .......... .......... .......... .......... .......... 20% 15.4M 9s
54600K .......... .......... .......... .......... .......... 20% 42.9M 9s
54650K .......... .......... .......... .......... .......... 20% 26.9M 9s
54700K .......... .......... .......... .......... .......... 20% 22.8M 9s
54750K .......... .......... .......... .......... .......... 20% 22.6M 9s
54800K .......... .......... .......... .......... .......... 20% 23.7M 9s
54850K .......... .......... .......... .......... .......... 20% 97.1M 9s
54900K .......... .......... .......... .......... .......... 20% 17.2M 9s
54950K .......... .......... .......... .......... .......... 20% 18.9M 9s
55000K .......... .......... .......... .......... .......... 20% 18.7M 9s
55050K .......... .......... .......... .......... .......... 20% 25.3M 9s
55100K .......... .......... .......... .......... .......... 20% 23.9M 9s
55150K .......... .......... .......... .......... .......... 20% 17.1M 9s
55200K .......... .......... .......... .......... .......... 20% 14.5M 9s
55250K .......... .......... .......... .......... .......... 20% 18.9M 9s
55300K .......... .......... .......... .......... .......... 20% 24.9M 9s
55350K .......... .......... .......... .......... .......... 20% 22.5M 9s
55400K .......... .......... .......... .......... .......... 20% 15.7M 9s
55450K .......... .......... .......... .......... .......... 20% 17.6M 9s
55500K .......... .......... .......... .......... .......... 20% 11.8M 9s
55550K .......... .......... .......... .......... .......... 20% 77.6M 9s
55600K .......... .......... .......... .......... .......... 20% 14.0M 9s
55650K .......... .......... .......... .......... .......... 20% 30.4M 9s
55700K .......... .......... .......... .......... .......... 20% 15.4M 9s
55750K .......... .......... .......... .......... .......... 20% 22.7M 9s
55800K .......... .......... .......... .......... .......... 21% 44.2M 9s
55850K .......... .......... .......... .......... .......... 21% 18.8M 9s
55900K .......... .......... .......... .......... .......... 21% 19.5M 9s
55950K .......... .......... .......... .......... .......... 21% 24.6M 9s
56000K .......... .......... .......... .......... .......... 21% 18.7M 9s
56050K .......... .......... .......... .......... .......... 21% 25.4M 9s
56100K .......... .......... .......... .......... .......... 21% 21.3M 9s
56150K .......... .......... .......... .......... .......... 21% 45.5M 9s
56200K .......... .......... .......... .......... .......... 21% 21.1M 9s
56250K .......... .......... .......... .......... .......... 21% 26.6M 9s
56300K .......... .......... .......... .......... .......... 21% 18.8M 9s
56350K .......... .......... .......... .......... .......... 21% 44.5M 9s
56400K .......... .......... .......... .......... .......... 21% 30.8M 9s
56450K .......... .......... .......... .......... .......... 21% 25.7M 9s
56500K .......... .......... .......... .......... .......... 21% 26.4M 9s
56550K .......... .......... .......... .......... .......... 21% 18.6M 9s
56600K .......... .......... .......... .......... .......... 21% 19.5M 9s
56650K .......... .......... .......... .......... .......... 21% 20.3M 9s
56700K .......... .......... .......... .......... .......... 21% 17.3M 9s
56750K .......... .......... .......... .......... .......... 21% 23.7M 9s
56800K .......... .......... .......... .......... .......... 21% 20.9M 9s
56850K .......... .......... .......... .......... .......... 21% 22.8M 9s
56900K .......... .......... .......... .......... .......... 21% 39.3M 9s
56950K .......... .......... .......... .......... .......... 21% 19.3M 9s
57000K .......... .......... .......... .......... .......... 21% 31.7M 9s
57050K .......... .......... .......... .......... .......... 21% 24.8M 9s
57100K .......... .......... .......... .......... .......... 21% 13.3M 9s
57150K .......... .......... .......... .......... .......... 21% 141M 9s
57200K .......... .......... .......... .......... .......... 21% 21.1M 9s
57250K .......... .......... .......... .......... .......... 21% 17.5M 9s
57300K .......... .......... .......... .......... .......... 21% 44.3M 9s
57350K .......... .......... .......... .......... .......... 21% 14.8M 9s
57400K .......... .......... .......... .......... .......... 21% 19.5M 9s
57450K .......... .......... .......... .......... .......... 21% 27.7M 9s
57500K .......... .......... .......... .......... .......... 21% 21.7M 9s
57550K .......... .......... .......... .......... .......... 21% 15.5M 9s
57600K .......... .......... .......... .......... .......... 21% 60.4M 9s
57650K .......... .......... .......... .......... .......... 21% 30.8M 9s
57700K .......... .......... .......... .......... .......... 21% 19.6M 9s
57750K .......... .......... .......... .......... .......... 21% 30.4M 9s
57800K .......... .......... .......... .......... .......... 21% 19.8M 9s
57850K .......... .......... .......... .......... .......... 21% 19.5M 9s
57900K .......... .......... .......... .......... .......... 21% 16.2M 9s
57950K .......... .......... .......... .......... .......... 21% 28.6M 9s
58000K .......... .......... .......... .......... .......... 21% 13.2M 9s
58050K .......... .......... .......... .......... .......... 21% 23.5M 9s
58100K .......... .......... .......... .......... .......... 21% 12.7M 9s
58150K .......... .......... .......... .......... .......... 21% 12.8M 9s
58200K .......... .......... .......... .......... .......... 21% 19.9M 9s
58250K .......... .......... .......... .......... .......... 21% 19.6M 9s
58300K .......... .......... .......... .......... .......... 21% 40.7M 9s
58350K .......... .......... .......... .......... .......... 21% 17.6M 9s
58400K .......... .......... .......... .......... .......... 21% 33.2M 9s
58450K .......... .......... .......... .......... .......... 22% 15.9M 9s
58500K .......... .......... .......... .......... .......... 22% 16.4M 9s
58550K .......... .......... .......... .......... .......... 22% 22.8M 9s
58600K .......... .......... .......... .......... .......... 22% 26.0M 9s
58650K .......... .......... .......... .......... .......... 22% 27.7M 9s
58700K .......... .......... .......... .......... .......... 22% 17.1M 9s
58750K .......... .......... .......... .......... .......... 22% 19.9M 9s
58800K .......... .......... .......... .......... .......... 22% 46.3M 9s
58850K .......... .......... .......... .......... .......... 22% 13.4M 9s
58900K .......... .......... .......... .......... .......... 22% 17.2M 9s
58950K .......... .......... .......... .......... .......... 22% 25.9M 9s
59000K .......... .......... .......... .......... .......... 22% 13.8M 9s
59050K .......... .......... .......... .......... .......... 22% 22.2M 9s
59100K .......... .......... .......... .......... .......... 22% 17.9M 9s
59150K .......... .......... .......... .......... .......... 22% 14.3M 9s
59200K .......... .......... .......... .......... .......... 22% 18.2M 9s
59250K .......... .......... .......... .......... .......... 22% 33.3M 9s
59300K .......... .......... .......... .......... .......... 22% 18.8M 9s
59350K .......... .......... .......... .......... .......... 22% 25.6M 9s
59400K .......... .......... .......... .......... .......... 22% 22.9M 9s
59450K .......... .......... .......... .......... .......... 22% 22.8M 9s
59500K .......... .......... .......... .......... .......... 22% 24.0M 9s
59550K .......... .......... .......... .......... .......... 22% 15.8M 9s
59600K .......... .......... .......... .......... .......... 22% 21.3M 9s
59650K .......... .......... .......... .......... .......... 22% 18.3M 9s
59700K .......... .......... .......... .......... .......... 22% 14.8M 9s
59750K .......... .......... .......... .......... .......... 22% 22.8M 9s
59800K .......... .......... .......... .......... .......... 22% 19.6M 9s
59850K .......... .......... .......... .......... .......... 22% 46.1M 9s
59900K .......... .......... .......... .......... .......... 22% 19.7M 9s
59950K .......... .......... .......... .......... .......... 22% 25.8M 9s
60000K .......... .......... .......... .......... .......... 22% 17.2M 9s
60050K .......... .......... .......... .......... .......... 22% 25.4M 9s
60100K .......... .......... .......... .......... .......... 22% 21.1M 9s
60150K .......... .......... .......... .......... .......... 22% 19.0M 9s
60200K .......... .......... .......... .......... .......... 22% 15.6M 9s
60250K .......... .......... .......... .......... .......... 22% 16.5M 9s
60300K .......... .......... .......... .......... .......... 22% 55.9M 9s
60350K .......... .......... .......... .......... .......... 22% 18.0M 9s
60400K .......... .......... .......... .......... .......... 22% 20.5M 9s
60450K .......... .......... .......... .......... .......... 22% 16.4M 9s
60500K .......... .......... .......... .......... .......... 22% 18.7M 9s
60550K .......... .......... .......... .......... .......... 22% 18.9M 9s
60600K .......... .......... .......... .......... .......... 22% 13.6M 9s
60650K .......... .......... .......... .......... .......... 22% 19.3M 9s
60700K .......... .......... .......... .......... .......... 22% 14.6M 9s
60750K .......... .......... .......... .......... .......... 22% 19.3M 9s
60800K .......... .......... .......... .......... .......... 22% 16.3M 9s
60850K .......... .......... .......... .......... .......... 22% 13.3M 9s
60900K .......... .......... .......... .......... .......... 22% 31.6M 9s
60950K .......... .......... .......... .......... .......... 22% 17.6M 9s
61000K .......... .......... .......... .......... .......... 22% 16.3M 9s
61050K .......... .......... .......... .......... .......... 22% 17.1M 9s
61100K .......... .......... .......... .......... .......... 23% 18.6M 9s
61150K .......... .......... .......... .......... .......... 23% 37.8M 9s
61200K .......... .......... .......... .......... .......... 23% 19.7M 9s
61250K .......... .......... .......... .......... .......... 23% 14.4M 9s
61300K .......... .......... .......... .......... .......... 23% 12.8M 9s
61350K .......... .......... .......... .......... .......... 23% 14.2M 9s
61400K .......... .......... .......... .......... .......... 23% 28.8M 9s
61450K .......... .......... .......... .......... .......... 23% 9.53M 9s
61500K .......... .......... .......... .......... .......... 23% 12.2M 9s
61550K .......... .......... .......... .......... .......... 23% 21.0M 9s
61600K .......... .......... .......... .......... .......... 23% 15.0M 9s
61650K .......... .......... .......... .......... .......... 23% 35.3M 9s
61700K .......... .......... .......... .......... .......... 23% 12.6M 9s
61750K .......... .......... .......... .......... .......... 23% 17.8M 9s
61800K .......... .......... .......... .......... .......... 23% 17.7M 9s
61850K .......... .......... .......... .......... .......... 23% 17.5M 9s
61900K .......... .......... .......... .......... .......... 23% 32.5M 9s
61950K .......... .......... .......... .......... .......... 23% 14.8M 9s
62000K .......... .......... .......... .......... .......... 23% 15.0M 9s
62050K .......... .......... .......... .......... .......... 23% 17.5M 9s
62100K .......... .......... .......... .......... .......... 23% 22.2M 9s
62150K .......... .......... .......... .......... .......... 23% 19.0M 9s
62200K .......... .......... .......... .......... .......... 23% 15.0M 9s
62250K .......... .......... .......... .......... .......... 23% 14.3M 9s
62300K .......... .......... .......... .......... .......... 23% 55.6M 9s
62350K .......... .......... .......... .......... .......... 23% 15.4M 9s
62400K .......... .......... .......... .......... .......... 23% 16.6M 9s
62450K .......... .......... .......... .......... .......... 23% 17.5M 9s
62500K .......... .......... .......... .......... .......... 23% 14.4M 9s
62550K .......... .......... .......... .......... .......... 23% 30.7M 9s
62600K .......... .......... .......... .......... .......... 23% 17.3M 9s
62650K .......... .......... .......... .......... .......... 23% 14.1M 9s
62700K .......... .......... .......... .......... .......... 23% 15.2M 9s
62750K .......... .......... .......... .......... .......... 23% 28.8M 9s
62800K .......... .......... .......... .......... .......... 23% 28.0M 9s
62850K .......... .......... .......... .......... .......... 23% 19.1M 9s
62900K .......... .......... .......... .......... .......... 23% 16.0M 9s
62950K .......... .......... .......... .......... .......... 23% 13.3M 9s
63000K .......... .......... .......... .......... .......... 23% 17.8M 9s
63050K .......... .......... .......... .......... .......... 23% 33.4M 9s
63100K .......... .......... .......... .......... .......... 23% 13.5M 9s
63150K .......... .......... .......... .......... .......... 23% 19.4M 9s
63200K .......... .......... .......... .......... .......... 23% 17.0M 9s
63250K .......... .......... .......... .......... .......... 23% 20.6M 9s
63300K .......... .......... .......... .......... .......... 23% 28.3M 9s
63350K .......... .......... .......... .......... .......... 23% 22.5M 9s
63400K .......... .......... .......... .......... .......... 23% 5.95M 9s
63450K .......... .......... .......... .......... .......... 23% 25.4M 9s
63500K .......... .......... .......... .......... .......... 23% 5.44M 9s
63550K .......... .......... .......... .......... .......... 23% 70.4M 9s
63600K .......... .......... .......... .......... .......... 23% 80.9M 9s
63650K .......... .......... .......... .......... .......... 23% 126M 9s
63700K .......... .......... .......... .......... .......... 23% 182M 9s
63750K .......... .......... .......... .......... .......... 24% 32.5M 9s
63800K .......... .......... .......... .......... .......... 24% 15.5M 9s
63850K .......... .......... .......... .......... .......... 24% 15.1M 9s
63900K .......... .......... .......... .......... .......... 24% 13.3M 9s
63950K .......... .......... .......... .......... .......... 24% 18.1M 9s
64000K .......... .......... .......... .......... .......... 24% 32.1M 9s
64050K .......... .......... .......... .......... .......... 24% 19.4M 9s
64100K .......... .......... .......... .......... .......... 24% 17.7M 9s
64150K .......... .......... .......... .......... .......... 24% 15.6M 9s
64200K .......... .......... .......... .......... .......... 24% 13.8M 9s
64250K .......... .......... .......... .......... .......... 24% 33.8M 9s
64300K .......... .......... .......... .......... .......... 24% 27.2M 9s
64350K .......... .......... .......... .......... .......... 24% 14.9M 9s
64400K .......... .......... .......... .......... .......... 24% 14.8M 9s
64450K .......... .......... .......... .......... .......... 24% 11.4M 9s
64500K .......... .......... .......... .......... .......... 24% 29.1M 9s
64550K .......... .......... .......... .......... .......... 24% 14.9M 9s
64600K .......... .......... .......... .......... .......... 24% 15.8M 9s
64650K .......... .......... .......... .......... .......... 24% 16.1M 9s
64700K .......... .......... .......... .......... .......... 24% 16.9M 9s
64750K .......... .......... .......... .......... .......... 24% 32.2M 9s
64800K .......... .......... .......... .......... .......... 24% 16.6M 9s
64850K .......... .......... .......... .......... .......... 24% 15.2M 9s
64900K .......... .......... .......... .......... .......... 24% 13.8M 9s
64950K .......... .......... .......... .......... .......... 24% 17.9M 9s
65000K .......... .......... .......... .......... .......... 24% 30.6M 9s
65050K .......... .......... .......... .......... .......... 24% 15.0M 9s
65100K .......... .......... .......... .......... .......... 24% 12.1M 9s
65150K .......... .......... .......... .......... .......... 24% 16.6M 9s
65200K .......... .......... .......... .......... .......... 24% 25.1M 9s
65250K .......... .......... .......... .......... .......... 24% 13.7M 9s
65300K .......... .......... .......... .......... .......... 24% 15.2M 9s
65350K .......... .......... .......... .......... .......... 24% 16.2M 9s
65400K .......... .......... .......... .......... .......... 24% 14.6M 9s
65450K .......... .......... .......... .......... .......... 24% 18.4M 9s
65500K .......... .......... .......... .......... .......... 24% 13.8M 9s
65550K .......... .......... .......... .......... .......... 24% 11.9M 9s
65600K .......... .......... .......... .......... .......... 24% 7.82M 9s
65650K .......... .......... .......... .......... .......... 24% 39.9M 9s
65700K .......... .......... .......... .......... .......... 24% 10.5M 9s
65750K .......... .......... .......... .......... .......... 24% 11.4M 9s
65800K .......... .......... .......... .......... .......... 24% 16.2M 9s
65850K .......... .......... .......... .......... .......... 24% 17.5M 9s
65900K .......... .......... .......... .......... .......... 24% 26.4M 9s
65950K .......... .......... .......... .......... .......... 24% 19.6M 9s
66000K .......... .......... .......... .......... .......... 24% 24.2M 9s
66050K .......... .......... .......... .......... .......... 24% 18.1M 9s
66100K .......... .......... .......... .......... .......... 24% 14.9M 9s
66150K .......... .......... .......... .......... .......... 24% 143M 9s
66200K .......... .......... .......... .......... .......... 24% 7.69M 9s
66250K .......... .......... .......... .......... .......... 24% 19.5M 9s
66300K .......... .......... .......... .......... .......... 24% 10.8M 9s
66350K .......... .......... .......... .......... .......... 24% 19.9M 9s
66400K .......... .......... .......... .......... .......... 25% 36.6M 9s
66450K .......... .......... .......... .......... .......... 25% 12.6M 9s
66500K .......... .......... .......... .......... .......... 25% 14.2M 9s
66550K .......... .......... .......... .......... .......... 25% 13.2M 9s
66600K .......... .......... .......... .......... .......... 25% 12.3M 9s
66650K .......... .......... .......... .......... .......... 25% 12.0M 9s
66700K .......... .......... .......... .......... .......... 25% 7.96M 9s
66750K .......... .......... .......... .......... .......... 25% 10.6M 9s
66800K .......... .......... .......... .......... .......... 25% 12.5M 9s
66850K .......... .......... .......... .......... .......... 25% 7.93M 9s
66900K .......... .......... .......... .......... .......... 25% 31.1M 9s
66950K .......... .......... .......... .......... .......... 25% 7.82M 9s
67000K .......... .......... .......... .......... .......... 25% 12.1M 9s
67050K .......... .......... .......... .......... .......... 25% 9.01M 9s
67100K .......... .......... .......... .......... .......... 25% 11.0M 9s
67150K .......... .......... .......... .......... .......... 25% 49.2M 9s
67200K .......... .......... .......... .......... .......... 25% 18.4M 9s
67250K .......... .......... .......... .......... .......... 25% 10.1M 9s
67300K .......... .......... .......... .......... .......... 25% 14.4M 9s
67350K .......... .......... .......... .......... .......... 25% 11.5M 9s
67400K .......... .......... .......... .......... .......... 25% 15.8M 9s
67450K .......... .......... .......... .......... .......... 25% 12.0M 9s
67500K .......... .......... .......... .......... .......... 25% 23.6M 9s
67550K .......... .......... .......... .......... .......... 25% 23.4M 9s
67600K .......... .......... .......... .......... .......... 25% 20.8M 9s
67650K .......... .......... .......... .......... .......... 25% 21.9M 9s
67700K .......... .......... .......... .......... .......... 25% 18.4M 9s
67750K .......... .......... .......... .......... .......... 25% 16.7M 9s
67800K .......... .......... .......... .......... .......... 25% 16.6M 9s
67850K .......... .......... .......... .......... .......... 25% 20.6M 9s
67900K .......... .......... .......... .......... .......... 25% 14.3M 9s
67950K .......... .......... .......... .......... .......... 25% 15.2M 9s
68000K .......... .......... .......... .......... .......... 25% 12.3M 9s
68050K .......... .......... .......... .......... .......... 25% 16.6M 9s
68100K .......... .......... .......... .......... .......... 25% 9.39M 9s
68150K .......... .......... .......... .......... .......... 25% 16.0M 9s
68200K .......... .......... .......... .......... .......... 25% 27.7M 9s
68250K .......... .......... .......... .......... .......... 25% 19.7M 9s
68300K .......... .......... .......... .......... .......... 25% 19.7M 9s
68350K .......... .......... .......... .......... .......... 25% 9.14M 9s
68400K .......... .......... .......... .......... .......... 25% 14.6M 9s
68450K .......... .......... .......... .......... .......... 25% 2.78M 9s
68500K .......... .......... .......... .......... .......... 25% 67.6M 9s
68550K .......... .......... .......... .......... .......... 25% 249M 9s
68600K .......... .......... .......... .......... .......... 25% 35.0M 9s
68650K .......... .......... .......... .......... .......... 25% 42.6M 9s
68700K .......... .......... .......... .......... .......... 25% 61.8M 9s
68750K .......... .......... .......... .......... .......... 25% 42.8M 9s
68800K .......... .......... .......... .......... .......... 25% 27.4M 9s
68850K .......... .......... .......... .......... .......... 25% 9.89M 9s
68900K .......... .......... .......... .......... .......... 25% 10.6M 9s
68950K .......... .......... .......... .......... .......... 25% 6.95M 9s
69000K .......... .......... .......... .......... .......... 25% 13.1M 9s
69050K .......... .......... .......... .......... .......... 26% 10.5M 9s
69100K .......... .......... .......... .......... .......... 26% 10.5M 9s
69150K .......... .......... .......... .......... .......... 26% 11.8M 9s
69200K .......... .......... .......... .......... .......... 26% 11.3M 9s
69250K .......... .......... .......... .......... .......... 26% 10.8M 9s
69300K .......... .......... .......... .......... .......... 26% 12.1M 9s
69350K .......... .......... .......... .......... .......... 26% 21.1M 9s
69400K .......... .......... .......... .......... .......... 26% 9.87M 9s
69450K .......... .......... .......... .......... .......... 26% 15.6M 9s
69500K .......... .......... .......... .......... .......... 26% 16.6M 9s
69550K .......... .......... .......... .......... .......... 26% 14.0M 9s
69600K .......... .......... .......... .......... .......... 26% 12.8M 9s
69650K .......... .......... .......... .......... .......... 26% 20.6M 9s
69700K .......... .......... .......... .......... .......... 26% 11.1M 9s
69750K .......... .......... .......... .......... .......... 26% 17.6M 9s
69800K .......... .......... .......... .......... .......... 26% 21.2M 9s
69850K .......... .......... .......... .......... .......... 26% 10.5M 9s
69900K .......... .......... .......... .......... .......... 26% 12.0M 9s
69950K .......... .......... .......... .......... .......... 26% 9.39M 9s
70000K .......... .......... .......... .......... .......... 26% 10.6M 9s
70050K .......... .......... .......... .......... .......... 26% 8.79M 9s
70100K .......... .......... .......... .......... .......... 26% 7.15M 9s
70150K .......... .......... .......... .......... .......... 26% 8.61M 9s
70200K .......... .......... .......... .......... .......... 26% 7.63M 9s
70250K .......... .......... .......... .......... .......... 26% 7.33M 9s
70300K .......... .......... .......... .......... .......... 26% 9.16M 9s
70350K .......... .......... .......... .......... .......... 26% 8.42M 9s
70400K .......... .......... .......... .......... .......... 26% 9.01M 9s
70450K .......... .......... .......... .......... .......... 26% 7.90M 9s
70500K .......... .......... .......... .......... .......... 26% 11.9M 9s
70550K .......... .......... .......... .......... .......... 26% 8.16M 9s
70600K .......... .......... .......... .......... .......... 26% 8.22M 9s
70650K .......... .......... .......... .......... .......... 26% 6.28M 9s
70700K .......... .......... .......... .......... .......... 26% 8.86M 9s
70750K .......... .......... .......... .......... .......... 26% 10.6M 9s
70800K .......... .......... .......... .......... .......... 26% 14.9M 9s
70850K .......... .......... .......... .......... .......... 26% 21.0M 9s
70900K .......... .......... .......... .......... .......... 26% 9.18M 9s
70950K .......... .......... .......... .......... .......... 26% 16.2M 9s
71000K .......... .......... .......... .......... .......... 26% 20.6M 9s
71050K .......... .......... .......... .......... .......... 26% 6.87M 9s
71100K .......... .......... .......... .......... .......... 26% 9.45M 9s
71150K .......... .......... .......... .......... .......... 26% 11.8M 9s
71200K .......... .......... .......... .......... .......... 26% 8.71M 9s
71250K .......... .......... .......... .......... .......... 26% 8.82M 9s
71300K .......... .......... .......... .......... .......... 26% 11.2M 9s
71350K .......... .......... .......... .......... .......... 26% 6.57M 9s
71400K .......... .......... .......... .......... .......... 26% 8.76M 9s
71450K .......... .......... .......... .......... .......... 26% 8.01M 9s
71500K .......... .......... .......... .......... .......... 26% 14.8M 9s
71550K .......... .......... .......... .......... .......... 26% 12.1M 9s
71600K .......... .......... .......... .......... .......... 26% 7.99M 9s
71650K .......... .......... .......... .......... .......... 26% 15.5M 9s
71700K .......... .......... .......... .......... .......... 26% 9.41M 9s
71750K .......... .......... .......... .......... .......... 27% 9.28M 9s
71800K .......... .......... .......... .......... .......... 27% 25.4M 9s
71850K .......... .......... .......... .......... .......... 27% 11.4M 9s
71900K .......... .......... .......... .......... .......... 27% 9.60M 9s
71950K .......... .......... .......... .......... .......... 27% 12.3M 9s
72000K .......... .......... .......... .......... .......... 27% 11.8M 9s
72050K .......... .......... .......... .......... .......... 27% 16.3M 9s
72100K .......... .......... .......... .......... .......... 27% 10.2M 9s
72150K .......... .......... .......... .......... .......... 27% 12.9M 9s
72200K .......... .......... .......... .......... .......... 27% 10.4M 9s
72250K .......... .......... .......... .......... .......... 27% 9.21M 9s
72300K .......... .......... .......... .......... .......... 27% 17.5M 9s
72350K .......... .......... .......... .......... .......... 27% 9.76M 9s
72400K .......... .......... .......... .......... .......... 27% 16.2M 9s
72450K .......... .......... .......... .......... .......... 27% 22.0M 9s
72500K .......... .......... .......... .......... .......... 27% 17.3M 9s
72550K .......... .......... .......... .......... .......... 27% 10.5M 9s
72600K .......... .......... .......... .......... .......... 27% 3.59M 9s
72650K .......... .......... .......... .......... .......... 27% 26.6M 9s
72700K .......... .......... .......... .......... .......... 27% 128M 9s
72750K .......... .......... .......... .......... .......... 27% 151M 9s
72800K .......... .......... .......... .......... .......... 27% 7.84M 9s
72850K .......... .......... .......... .......... .......... 27% 13.0M 9s
72900K .......... .......... .......... .......... .......... 27% 5.78M 9s
72950K .......... .......... .......... .......... .......... 27% 12.5M 9s
73000K .......... .......... .......... .......... .......... 27% 11.5M 9s
73050K .......... .......... .......... .......... .......... 27% 6.89M 9s
73100K .......... .......... .......... .......... .......... 27% 13.5M 9s
73150K .......... .......... .......... .......... .......... 27% 8.75M 9s
73200K .......... .......... .......... .......... .......... 27% 13.7M 9s
73250K .......... .......... .......... .......... .......... 27% 8.92M 9s
73300K .......... .......... .......... .......... .......... 27% 14.6M 9s
73350K .......... .......... .......... .......... .......... 27% 6.01M 9s
73400K .......... .......... .......... .......... .......... 27% 11.3M 9s
73450K .......... .......... .......... .......... .......... 27% 6.21M 9s
73500K .......... .......... .......... .......... .......... 27% 11.6M 9s
73550K .......... .......... .......... .......... .......... 27% 6.93M 9s
73600K .......... .......... .......... .......... .......... 27% 11.3M 9s
73650K .......... .......... .......... .......... .......... 27% 7.83M 9s
73700K .......... .......... .......... .......... .......... 27% 15.7M 9s
73750K .......... .......... .......... .......... .......... 27% 6.91M 9s
73800K .......... .......... .......... .......... .......... 27% 17.3M 9s
73850K .......... .......... .......... .......... .......... 27% 9.65M 9s
73900K .......... .......... .......... .......... .......... 27% 10.6M 9s
73950K .......... .......... .......... .......... .......... 27% 10.4M 9s
74000K .......... .......... .......... .......... .......... 27% 12.6M 9s
74050K .......... .......... .......... .......... .......... 27% 13.0M 9s
74100K .......... .......... .......... .......... .......... 27% 9.51M 9s
74150K .......... .......... .......... .......... .......... 27% 13.4M 9s
74200K .......... .......... .......... .......... .......... 27% 8.24M 9s
74250K .......... .......... .......... .......... .......... 27% 19.7M 9s
74300K .......... .......... .......... .......... .......... 27% 7.10M 9s
74350K .......... .......... .......... .......... .......... 27% 15.1M 9s
74400K .......... .......... .......... .......... .......... 28% 8.45M 9s
74450K .......... .......... .......... .......... .......... 28% 11.3M 9s
74500K .......... .......... .......... .......... .......... 28% 16.3M 9s
74550K .......... .......... .......... .......... .......... 28% 9.12M 9s
74600K .......... .......... .......... .......... .......... 28% 11.3M 9s
74650K .......... .......... .......... .......... .......... 28% 8.27M 9s
74700K .......... .......... .......... .......... .......... 28% 10.9M 9s
74750K .......... .......... .......... .......... .......... 28% 10.5M 9s
74800K .......... .......... .......... .......... .......... 28% 9.52M 9s
74850K .......... .......... .......... .......... .......... 28% 10.4M 9s
74900K .......... .......... .......... .......... .......... 28% 8.11M 9s
74950K .......... .......... .......... .......... .......... 28% 13.7M 9s
75000K .......... .......... .......... .......... .......... 28% 10.0M 9s
75050K .......... .......... .......... .......... .......... 28% 10.1M 9s
75100K .......... .......... .......... .......... .......... 28% 8.88M 9s
75150K .......... .......... .......... .......... .......... 28% 12.6M 9s
75200K .......... .......... .......... .......... .......... 28% 9.31M 9s
75250K .......... .......... .......... .......... .......... 28% 9.93M 9s
75300K .......... .......... .......... .......... .......... 28% 17.7M 9s
75350K .......... .......... .......... .......... .......... 28% 9.10M 9s
75400K .......... .......... .......... .......... .......... 28% 9.72M 9s
75450K .......... .......... .......... .......... .......... 28% 8.98M 9s
75500K .......... .......... .......... .......... .......... 28% 12.1M 9s
75550K .......... .......... .......... .......... .......... 28% 13.9M 9s
75600K .......... .......... .......... .......... .......... 28% 8.04M 9s
75650K .......... .......... .......... .......... .......... 28% 15.2M 9s
75700K .......... .......... .......... .......... .......... 28% 10.0M 9s
75750K .......... .......... .......... .......... .......... 28% 11.3M 9s
75800K .......... .......... .......... .......... .......... 28% 8.63M 9s
75850K .......... .......... .......... .......... .......... 28% 18.2M 9s
75900K .......... .......... .......... .......... .......... 28% 8.93M 9s
75950K .......... .......... .......... .......... .......... 28% 11.1M 9s
76000K .......... .......... .......... .......... .......... 28% 9.23M 9s
76050K .......... .......... .......... .......... .......... 28% 11.6M 9s
76100K .......... .......... .......... .......... .......... 28% 16.9M 9s
76150K .......... .......... .......... .......... .......... 28% 9.50M 9s
76200K .......... .......... .......... .......... .......... 28% 11.2M 9s
76250K .......... .......... .......... .......... .......... 28% 8.86M 9s
76300K .......... .......... .......... .......... .......... 28% 11.2M 9s
76350K .......... .......... .......... .......... .......... 28% 12.6M 9s
76400K .......... .......... .......... .......... .......... 28% 8.91M 9s
76450K .......... .......... .......... .......... .......... 28% 12.5M 9s
76500K .......... .......... .......... .......... .......... 28% 13.1M 9s
76550K .......... .......... .......... .......... .......... 28% 7.69M 9s
76600K .......... .......... .......... .......... .......... 28% 14.2M 9s
76650K .......... .......... .......... .......... .......... 28% 9.79M 9s
76700K .......... .......... .......... .......... .......... 28% 10.4M 9s
76750K .......... .......... .......... .......... .......... 28% 15.9M 9s
76800K .......... .......... .......... .......... .......... 28% 7.18M 9s
76850K .......... .......... .......... .......... .......... 28% 17.5M 9s
76900K .......... .......... .......... .......... .......... 28% 11.1M 9s
76950K .......... .......... .......... .......... .......... 28% 8.47M 9s
77000K .......... .......... .......... .......... .......... 28% 17.5M 9s
77050K .......... .......... .......... .......... .......... 29% 8.98M 9s
77100K .......... .......... .......... .......... .......... 29% 10.1M 9s
77150K .......... .......... .......... .......... .......... 29% 11.1M 9s
77200K .......... .......... .......... .......... .......... 29% 8.83M 9s
77250K .......... .......... .......... .......... .......... 29% 15.8M 9s
77300K .......... .......... .......... .......... .......... 29% 11.2M 9s
77350K .......... .......... .......... .......... .......... 29% 8.10M 9s
77400K .......... .......... .......... .......... .......... 29% 14.5M 9s
77450K .......... .......... .......... .......... .......... 29% 7.51M 9s
77500K .......... .......... .......... .......... .......... 29% 14.5M 9s
77550K .......... .......... .......... .......... .......... 29% 11.7M 9s
77600K .......... .......... .......... .......... .......... 29% 9.13M 9s
77650K .......... .......... .......... .......... .......... 29% 11.9M 9s
77700K .......... .......... .......... .......... .......... 29% 8.52M 9s
77750K .......... .......... .......... .......... .......... 29% 13.1M 9s
77800K .......... .......... .......... .......... .......... 29% 9.41M 9s
77850K .......... .......... .......... .......... .......... 29% 9.29M 9s
77900K .......... .......... .......... .......... .......... 29% 11.8M 9s
77950K .......... .......... .......... .......... .......... 29% 8.49M 9s
78000K .......... .......... .......... .......... .......... 29% 13.6M 9s
78050K .......... .......... .......... .......... .......... 29% 12.3M 9s
78100K .......... .......... .......... .......... .......... 29% 7.37M 9s
78150K .......... .......... .......... .......... .......... 29% 16.8M 9s
78200K .......... .......... .......... .......... .......... 29% 9.73M 9s
78250K .......... .......... .......... .......... .......... 29% 9.09M 10s
78300K .......... .......... .......... .......... .......... 29% 13.6M 10s
78350K .......... .......... .......... .......... .......... 29% 9.19M 10s
78400K .......... .......... .......... .......... .......... 29% 10.6M 10s
78450K .......... .......... .......... .......... .......... 29% 11.7M 10s
78500K .......... .......... .......... .......... .......... 29% 7.16M 10s
78550K .......... .......... .......... .......... .......... 29% 32.0M 10s
78600K .......... .......... .......... .......... .......... 29% 9.41M 10s
78650K .......... .......... .......... .......... .......... 29% 7.90M 10s
78700K .......... .......... .......... .......... .......... 29% 15.0M 10s
78750K .......... .......... .......... .......... .......... 29% 10.9M 10s
78800K .......... .......... .......... .......... .......... 29% 8.68M 10s
78850K .......... .......... .......... .......... .......... 29% 12.8M 10s
78900K .......... .......... .......... .......... .......... 29% 10.5M 10s
78950K .......... .......... .......... .......... .......... 29% 9.89M 10s
79000K .......... .......... .......... .......... .......... 29% 10.6M 10s
79050K .......... .......... .......... .......... .......... 29% 10.0M 10s
79100K .......... .......... .......... .......... .......... 29% 10.0M 10s
79150K .......... .......... .......... .......... .......... 29% 15.1M 10s
79200K .......... .......... .......... .......... .......... 29% 7.31M 10s
79250K .......... .......... .......... .......... .......... 29% 14.8M 10s
79300K .......... .......... .......... .......... .......... 29% 10.1M 10s
79350K .......... .......... .......... .......... .......... 29% 9.75M 10s
79400K .......... .......... .......... .......... .......... 29% 16.9M 10s
79450K .......... .......... .......... .......... .......... 29% 7.30M 10s
79500K .......... .......... .......... .......... .......... 29% 14.0M 10s
79550K .......... .......... .......... .......... .......... 29% 17.5M 10s
79600K .......... .......... .......... .......... .......... 29% 7.55M 10s
79650K .......... .......... .......... .......... .......... 29% 17.0M 10s
79700K .......... .......... .......... .......... .......... 30% 11.3M 10s
79750K .......... .......... .......... .......... .......... 30% 7.62M 10s
79800K .......... .......... .......... .......... .......... 30% 23.0M 10s
79850K .......... .......... .......... .......... .......... 30% 10.5M 10s
79900K .......... .......... .......... .......... .......... 30% 8.75M 10s
79950K .......... .......... .......... .......... .......... 30% 15.5M 10s
80000K .......... .......... .......... .......... .......... 30% 12.0M 10s
80050K .......... .......... .......... .......... .......... 30% 8.67M 10s
80100K .......... .......... .......... .......... .......... 30% 15.1M 10s
80150K .......... .......... .......... .......... .......... 30% 11.0M 10s
80200K .......... .......... .......... .......... .......... 30% 8.96M 10s
80250K .......... .......... .......... .......... .......... 30% 17.3M 10s
80300K .......... .......... .......... .......... .......... 30% 9.03M 10s
80350K .......... .......... .......... .......... .......... 30% 10.2M 10s
80400K .......... .......... .......... .......... .......... 30% 14.6M 10s
80450K .......... .......... .......... .......... .......... 30% 10.1M 10s
80500K .......... .......... .......... .......... .......... 30% 12.4M 10s
80550K .......... .......... .......... .......... .......... 30% 13.4M 10s
80600K .......... .......... .......... .......... .......... 30% 6.57M 10s
80650K .......... .......... .......... .......... .......... 30% 32.4M 10s
80700K .......... .......... .......... .......... .......... 30% 15.1M 10s
80750K .......... .......... .......... .......... .......... 30% 6.36M 10s
80800K .......... .......... .......... .......... .......... 30% 33.0M 10s
80850K .......... .......... .......... .......... .......... 30% 14.1M 10s
80900K .......... .......... .......... .......... .......... 30% 9.77M 10s
80950K .......... .......... .......... .......... .......... 30% 11.7M 10s
81000K .......... .......... .......... .......... .......... 30% 15.7M 10s
81050K .......... .......... .......... .......... .......... 30% 6.28M 10s
81100K .......... .......... .......... .......... .......... 30% 14.5M 10s
81150K .......... .......... .......... .......... .......... 30% 30.5M 10s
81200K .......... .......... .......... .......... .......... 30% 6.07M 10s
81250K .......... .......... .......... .......... .......... 30% 22.4M 10s
81300K .......... .......... .......... .......... .......... 30% 19.4M 10s
81350K .......... .......... .......... .......... .......... 30% 7.99M 10s
81400K .......... .......... .......... .......... .......... 30% 12.2M 10s
81450K .......... .......... .......... .......... .......... 30% 16.5M 10s
81500K .......... .......... .......... .......... .......... 30% 6.20M 10s
81550K .......... .......... .......... .......... .......... 30% 31.2M 10s
81600K .......... .......... .......... .......... .......... 30% 18.0M 10s
81650K .......... .......... .......... .......... .......... 30% 7.43M 10s
81700K .......... .......... .......... .......... .......... 30% 6.38M 10s
81750K .......... .......... .......... .......... .......... 30% 47.5M 10s
81800K .......... .......... .......... .......... .......... 30% 22.7M 10s
81850K .......... .......... .......... .......... .......... 30% 8.70M 10s
81900K .......... .......... .......... .......... .......... 30% 16.8M 10s
81950K .......... .......... .......... .......... .......... 30% 10.3M 10s
82000K .......... .......... .......... .......... .......... 30% 9.49M 10s
82050K .......... .......... .......... .......... .......... 30% 15.3M 10s
82100K .......... .......... .......... .......... .......... 30% 10.6M 10s
82150K .......... .......... .......... .......... .......... 30% 9.14M 10s
82200K .......... .......... .......... .......... .......... 30% 15.6M 10s
82250K .......... .......... .......... .......... .......... 30% 8.79M 10s
82300K .......... .......... .......... .......... .......... 30% 13.0M 10s
82350K .......... .......... .......... .......... .......... 31% 13.4M 10s
82400K .......... .......... .......... .......... .......... 31% 12.4M 10s
82450K .......... .......... .......... .......... .......... 31% 8.87M 10s
82500K .......... .......... .......... .......... .......... 31% 15.9M 10s
82550K .......... .......... .......... .......... .......... 31% 12.5M 10s
82600K .......... .......... .......... .......... .......... 31% 9.31M 10s
82650K .......... .......... .......... .......... .......... 31% 16.0M 10s
82700K .......... .......... .......... .......... .......... 31% 15.2M 10s
82750K .......... .......... .......... .......... .......... 31% 8.63M 10s
82800K .......... .......... .......... .......... .......... 31% 16.6M 10s
82850K .......... .......... .......... .......... .......... 31% 17.8M 10s
82900K .......... .......... .......... .......... .......... 31% 8.49M 10s
82950K .......... .......... .......... .......... .......... 31% 11.3M 10s
83000K .......... .......... .......... .......... .......... 31% 25.8M 10s
83050K .......... .......... .......... .......... .......... 31% 9.40M 10s
83100K .......... .......... .......... .......... .......... 31% 9.17M 10s
83150K .......... .......... .......... .......... .......... 31% 19.0M 10s
83200K .......... .......... .......... .......... .......... 31% 9.66M 10s
83250K .......... .......... .......... .......... .......... 31% 13.3M 10s
83300K .......... .......... .......... .......... .......... 31% 13.4M 10s
83350K .......... .......... .......... .......... .......... 31% 15.0M 10s
83400K .......... .......... .......... .......... .......... 31% 9.80M 10s
83450K .......... .......... .......... .......... .......... 31% 10.8M 10s
83500K .......... .......... .......... .......... .......... 31% 21.5M 10s
83550K .......... .......... .......... .......... .......... 31% 10.5M 10s
83600K .......... .......... .......... .......... .......... 31% 12.5M 10s
83650K .......... .......... .......... .......... .......... 31% 11.5M 10s
83700K .......... .......... .......... .......... .......... 31% 14.3M 10s
83750K .......... .......... .......... .......... .......... 31% 10.2M 10s
83800K .......... .......... .......... .......... .......... 31% 15.2M 10s
83850K .......... .......... .......... .......... .......... 31% 10.7M 10s
83900K .......... .......... .......... .......... .......... 31% 9.32M 10s
83950K .......... .......... .......... .......... .......... 31% 17.8M 10s
84000K .......... .......... .......... .......... .......... 31% 18.9M 10s
84050K .......... .......... .......... .......... .......... 31% 8.39M 10s
84100K .......... .......... .......... .......... .......... 31% 10.8M 10s
84150K .......... .......... .......... .......... .......... 31% 19.0M 10s
84200K .......... .......... .......... .......... .......... 31% 11.0M 10s
84250K .......... .......... .......... .......... .......... 31% 8.84M 10s
84300K .......... .......... .......... .......... .......... 31% 36.9M 10s
84350K .......... .......... .......... .......... .......... 31% 9.75M 10s
84400K .......... .......... .......... .......... .......... 31% 7.89M 10s
84450K .......... .......... .......... .......... .......... 31% 15.3M 10s
84500K .......... .......... .......... .......... .......... 31% 16.7M 10s
84550K .......... .......... .......... .......... .......... 31% 12.5M 10s
84600K .......... .......... .......... .......... .......... 31% 10.2M 10s
84650K .......... .......... .......... .......... .......... 31% 20.6M 10s
84700K .......... .......... .......... .......... .......... 31% 8.12M 10s
84750K .......... .......... .......... .......... .......... 31% 12.4M 10s
84800K .......... .......... .......... .......... .......... 31% 38.6M 10s
84850K .......... .......... .......... .......... .......... 31% 8.38M 10s
84900K .......... .......... .......... .......... .......... 31% 10.3M 10s
84950K .......... .......... .......... .......... .......... 31% 28.4M 10s
85000K .......... .......... .......... .......... .......... 32% 12.3M 10s
85050K .......... .......... .......... .......... .......... 32% 11.6M 10s
85100K .......... .......... .......... .......... .......... 32% 19.7M 10s
85150K .......... .......... .......... .......... .......... 32% 22.9M 10s
85200K .......... .......... .......... .......... .......... 32% 9.29M 10s
85250K .......... .......... .......... .......... .......... 32% 3.19M 10s
85300K .......... .......... .......... .......... .......... 32% 29.1M 10s
85350K .......... .......... .......... .......... .......... 32% 75.2M 10s
85400K .......... .......... .......... .......... .......... 32% 92.5M 10s
85450K .......... .......... .......... .......... .......... 32% 42.2M 10s
85500K .......... .......... .......... .......... .......... 32% 11.0M 10s
85550K .......... .......... .......... .......... .......... 32% 39.3M 10s
85600K .......... .......... .......... .......... .......... 32% 8.03M 10s
85650K .......... .......... .......... .......... .......... 32% 13.1M 10s
85700K .......... .......... .......... .......... .......... 32% 12.6M 10s
85750K .......... .......... .......... .......... .......... 32% 8.39M 10s
85800K .......... .......... .......... .......... .......... 32% 30.2M 10s
85850K .......... .......... .......... .......... .......... 32% 6.47M 10s
85900K .......... .......... .......... .......... .......... 32% 33.0M 10s
85950K .......... .......... .......... .......... .......... 32% 8.49M 10s
86000K .......... .......... .......... .......... .......... 32% 11.8M 10s
86050K .......... .......... .......... .......... .......... 32% 14.0M 10s
86100K .......... .......... .......... .......... .......... 32% 7.95M 10s
86150K .......... .......... .......... .......... .......... 32% 19.4M 10s
86200K .......... .......... .......... .......... .......... 32% 6.41M 10s
86250K .......... .......... .......... .......... .......... 32% 31.1M 10s
86300K .......... .......... .......... .......... .......... 32% 10.7M 10s
86350K .......... .......... .......... .......... .......... 32% 11.1M 10s
86400K .......... .......... .......... .......... .......... 32% 10.0M 10s
86450K .......... .......... .......... .......... .......... 32% 9.28M 10s
86500K .......... .......... .......... .......... .......... 32% 20.5M 10s
86550K .......... .......... .......... .......... .......... 32% 11.7M 10s
86600K .......... .......... .......... .......... .......... 32% 9.49M 10s
86650K .......... .......... .......... .......... .......... 32% 9.34M 10s
86700K .......... .......... .......... .......... .......... 32% 10.8M 10s
86750K .......... .......... .......... .......... .......... 32% 13.8M 10s
86800K .......... .......... .......... .......... .......... 32% 12.6M 10s
86850K .......... .......... .......... .......... .......... 32% 9.98M 10s
86900K .......... .......... .......... .......... .......... 32% 15.8M 10s
86950K .......... .......... .......... .......... .......... 32% 8.87M 10s
87000K .......... .......... .......... .......... .......... 32% 11.2M 10s
87050K .......... .......... .......... .......... .......... 32% 16.6M 10s
87100K .......... .......... .......... .......... .......... 32% 12.3M 10s
87150K .......... .......... .......... .......... .......... 32% 12.1M 10s
87200K .......... .......... .......... .......... .......... 32% 9.77M 10s
87250K .......... .......... .......... .......... .......... 32% 18.1M 10s
87300K .......... .......... .......... .......... .......... 32% 9.86M 10s
87350K .......... .......... .......... .......... .......... 32% 11.8M 10s
87400K .......... .......... .......... .......... .......... 32% 14.0M 10s
87450K .......... .......... .......... .......... .......... 32% 9.11M 10s
87500K .......... .......... .......... .......... .......... 32% 11.1M 10s
87550K .......... .......... .......... .......... .......... 32% 23.9M 10s
87600K .......... .......... .......... .......... .......... 32% 8.94M 10s
87650K .......... .......... .......... .......... .......... 33% 13.8M 10s
87700K .......... .......... .......... .......... .......... 33% 9.64M 10s
87750K .......... .......... .......... .......... .......... 33% 8.57M 10s
87800K .......... .......... .......... .......... .......... 33% 51.1M 10s
87850K .......... .......... .......... .......... .......... 33% 8.54M 10s
87900K .......... .......... .......... .......... .......... 33% 11.8M 10s
87950K .......... .......... .......... .......... .......... 33% 10.1M 10s
88000K .......... .......... .......... .......... .......... 33% 14.8M 10s
88050K .......... .......... .......... .......... .......... 33% 14.7M 10s
88100K .......... .......... .......... .......... .......... 33% 10.4M 10s
88150K .......... .......... .......... .......... .......... 33% 9.62M 10s
88200K .......... .......... .......... .......... .......... 33% 8.86M 10s
88250K .......... .......... .......... .......... .......... 33% 16.8M 10s
88300K .......... .......... .......... .......... .......... 33% 12.9M 10s
88350K .......... .......... .......... .......... .......... 33% 10.2M 10s
88400K .......... .......... .......... .......... .......... 33% 8.04M 10s
88450K .......... .......... .......... .......... .......... 33% 13.3M 10s
88500K .......... .......... .......... .......... .......... 33% 14.7M 10s
88550K .......... .......... .......... .......... .......... 33% 15.7M 10s
88600K .......... .......... .......... .......... .......... 33% 9.98M 10s
88650K .......... .......... .......... .......... .......... 33% 10.6M 10s
88700K .......... .......... .......... .......... .......... 33% 12.8M 10s
88750K .......... .......... .......... .......... .......... 33% 12.3M 10s
88800K .......... .......... .......... .......... .......... 33% 10.4M 10s
88850K .......... .......... .......... .......... .......... 33% 9.88M 10s
88900K .......... .......... .......... .......... .......... 33% 10.1M 10s
88950K .......... .......... .......... .......... .......... 33% 13.8M 10s
89000K .......... .......... .......... .......... .......... 33% 11.4M 10s
89050K .......... .......... .......... .......... .......... 33% 8.09M 10s
89100K .......... .......... .......... .......... .......... 33% 16.0M 10s
89150K .......... .......... .......... .......... .......... 33% 14.1M 10s
89200K .......... .......... .......... .......... .......... 33% 11.9M 10s
89250K .......... .......... .......... .......... .......... 33% 11.8M 10s
89300K .......... .......... .......... .......... .......... 33% 10.0M 10s
89350K .......... .......... .......... .......... .......... 33% 17.5M 10s
89400K .......... .......... .......... .......... .......... 33% 11.7M 10s
89450K .......... .......... .......... .......... .......... 33% 9.14M 10s
89500K .......... .......... .......... .......... .......... 33% 13.3M 10s
89550K .......... .......... .......... .......... .......... 33% 20.4M 10s
89600K .......... .......... .......... .......... .......... 33% 8.86M 10s
89650K .......... .......... .......... .......... .......... 33% 12.2M 10s
89700K .......... .......... .......... .......... .......... 33% 7.25M 10s
89750K .......... .......... .......... .......... .......... 33% 19.7M 10s
89800K .......... .......... .......... .......... .......... 33% 10.9M 10s
89850K .......... .......... .......... .......... .......... 33% 11.3M 10s
89900K .......... .......... .......... .......... .......... 33% 17.3M 10s
89950K .......... .......... .......... .......... .......... 33% 11.0M 10s
90000K .......... .......... .......... .......... .......... 33% 12.7M 10s
90050K .......... .......... .......... .......... .......... 33% 16.9M 10s
90100K .......... .......... .......... .......... .......... 33% 10.9M 10s
90150K .......... .......... .......... .......... .......... 33% 8.57M 10s
90200K .......... .......... .......... .......... .......... 33% 29.4M 10s
90250K .......... .......... .......... .......... .......... 33% 8.83M 10s
90300K .......... .......... .......... .......... .......... 33% 14.3M 10s
90350K .......... .......... .......... .......... .......... 34% 24.1M 10s
90400K .......... .......... .......... .......... .......... 34% 8.84M 10s
90450K .......... .......... .......... .......... .......... 34% 12.2M 10s
90500K .......... .......... .......... .......... .......... 34% 23.6M 10s
90550K .......... .......... .......... .......... .......... 34% 12.9M 10s
90600K .......... .......... .......... .......... .......... 34% 11.4M 10s
90650K .......... .......... .......... .......... .......... 34% 14.1M 10s
90700K .......... .......... .......... .......... .......... 34% 14.6M 10s
90750K .......... .......... .......... .......... .......... 34% 17.1M 10s
90800K .......... .......... .......... .......... .......... 34% 14.9M 10s
90850K .......... .......... .......... .......... .......... 34% 8.70M 10s
90900K .......... .......... .......... .......... .......... 34% 13.7M 10s
90950K .......... .......... .......... .......... .......... 34% 26.7M 10s
91000K .......... .......... .......... .......... .......... 34% 7.91M 10s
91050K .......... .......... .......... .......... .......... 34% 13.8M 10s
91100K .......... .......... .......... .......... .......... 34% 10.7M 10s
91150K .......... .......... .......... .......... .......... 34% 12.2M 10s
91200K .......... .......... .......... .......... .......... 34% 11.4M 10s
91250K .......... .......... .......... .......... .......... 34% 19.2M 10s
91300K .......... .......... .......... .......... .......... 34% 14.8M 10s
91350K .......... .......... .......... .......... .......... 34% 12.1M 10s
91400K .......... .......... .......... .......... .......... 34% 14.8M 10s
91450K .......... .......... .......... .......... .......... 34% 9.85M 10s
91500K .......... .......... .......... .......... .......... 34% 18.6M 10s
91550K .......... .......... .......... .......... .......... 34% 11.3M 10s
91600K .......... .......... .......... .......... .......... 34% 13.9M 10s
91650K .......... .......... .......... .......... .......... 34% 12.5M 10s
91700K .......... .......... .......... .......... .......... 34% 12.9M 10s
91750K .......... .......... .......... .......... .......... 34% 7.94M 10s
91800K .......... .......... .......... .......... .......... 34% 15.3M 10s
91850K .......... .......... .......... .......... .......... 34% 10.5M 10s
91900K .......... .......... .......... .......... .......... 34% 14.7M 10s
91950K .......... .......... .......... .......... .......... 34% 14.7M 10s
92000K .......... .......... .......... .......... .......... 34% 14.1M 10s
92050K .......... .......... .......... .......... .......... 34% 13.5M 10s
92100K .......... .......... .......... .......... .......... 34% 15.3M 10s
92150K .......... .......... .......... .......... .......... 34% 11.5M 10s
92200K .......... .......... .......... .......... .......... 34% 16.8M 10s
92250K .......... .......... .......... .......... .......... 34% 18.5M 10s
92300K .......... .......... .......... .......... .......... 34% 10.7M 10s
92350K .......... .......... .......... .......... .......... 34% 21.4M 10s
92400K .......... .......... .......... .......... .......... 34% 11.9M 10s
92450K .......... .......... .......... .......... .......... 34% 7.72M 10s
92500K .......... .......... .......... .......... .......... 34% 9.99M 10s
92550K .......... .......... .......... .......... .......... 34% 15.9M 10s
92600K .......... .......... .......... .......... .......... 34% 9.82M 10s
92650K .......... .......... .......... .......... .......... 34% 13.6M 10s
92700K .......... .......... .......... .......... .......... 34% 12.7M 10s
92750K .......... .......... .......... .......... .......... 34% 17.1M 10s
92800K .......... .......... .......... .......... .......... 34% 10.2M 10s
92850K .......... .......... .......... .......... .......... 34% 19.8M 10s
92900K .......... .......... .......... .......... .......... 34% 14.6M 10s
92950K .......... .......... .......... .......... .......... 34% 14.9M 10s
93000K .......... .......... .......... .......... .......... 35% 9.47M 10s
93050K .......... .......... .......... .......... .......... 35% 20.2M 10s
93100K .......... .......... .......... .......... .......... 35% 13.1M 10s
93150K .......... .......... .......... .......... .......... 35% 10.6M 10s
93200K .......... .......... .......... .......... .......... 35% 23.8M 10s
93250K .......... .......... .......... .......... .......... 35% 12.9M 10s
93300K .......... .......... .......... .......... .......... 35% 9.07M 10s
93350K .......... .......... .......... .......... .......... 35% 9.31M 10s
93400K .......... .......... .......... .......... .......... 35% 8.97M 10s
93450K .......... .......... .......... .......... .......... 35% 7.45M 10s
93500K .......... .......... .......... .......... .......... 35% 18.0M 10s
93550K .......... .......... .......... .......... .......... 35% 20.4M 10s
93600K .......... .......... .......... .......... .......... 35% 13.1M 10s
93650K .......... .......... .......... .......... .......... 35% 10.2M 10s
93700K .......... .......... .......... .......... .......... 35% 19.0M 10s
93750K .......... .......... .......... .......... .......... 35% 11.2M 10s
93800K .......... .......... .......... .......... .......... 35% 20.0M 10s
93850K .......... .......... .......... .......... .......... 35% 15.3M 10s
93900K .......... .......... .......... .......... .......... 35% 9.01M 10s
93950K .......... .......... .......... .......... .......... 35% 8.48M 10s
94000K .......... .......... .......... .......... .......... 35% 9.62M 10s
94050K .......... .......... .......... .......... .......... 35% 15.0M 10s
94100K .......... .......... .......... .......... .......... 35% 18.7M 10s
94150K .......... .......... .......... .......... .......... 35% 9.51M 10s
94200K .......... .......... .......... .......... .......... 35% 11.4M 10s
94250K .......... .......... .......... .......... .......... 35% 23.9M 10s
94300K .......... .......... .......... .......... .......... 35% 11.9M 10s
94350K .......... .......... .......... .......... .......... 35% 9.97M 10s
94400K .......... .......... .......... .......... .......... 35% 10.1M 10s
94450K .......... .......... .......... .......... .......... 35% 10.3M 10s
94500K .......... .......... .......... .......... .......... 35% 9.74M 10s
94550K .......... .......... .......... .......... .......... 35% 25.4M 10s
94600K .......... .......... .......... .......... .......... 35% 11.9M 10s
94650K .......... .......... .......... .......... .......... 35% 8.60M 10s
94700K .......... .......... .......... .......... .......... 35% 13.5M 10s
94750K .......... .......... .......... .......... .......... 35% 9.54M 10s
94800K .......... .......... .......... .......... .......... 35% 13.2M 10s
94850K .......... .......... .......... .......... .......... 35% 13.0M 10s
94900K .......... .......... .......... .......... .......... 35% 15.5M 10s
94950K .......... .......... .......... .......... .......... 35% 10.1M 10s
95000K .......... .......... .......... .......... .......... 35% 15.7M 10s
95050K .......... .......... .......... .......... .......... 35% 12.4M 10s
95100K .......... .......... .......... .......... .......... 35% 11.2M 10s
95150K .......... .......... .......... .......... .......... 35% 13.3M 10s
95200K .......... .......... .......... .......... .......... 35% 11.0M 10s
95250K .......... .......... .......... .......... .......... 35% 11.2M 10s
95300K .......... .......... .......... .......... .......... 35% 22.0M 10s
95350K .......... .......... .......... .......... .......... 35% 9.93M 10s
95400K .......... .......... .......... .......... .......... 35% 10.9M 10s
95450K .......... .......... .......... .......... .......... 35% 22.7M 10s
95500K .......... .......... .......... .......... .......... 35% 10.3M 10s
95550K .......... .......... .......... .......... .......... 35% 11.5M 10s
95600K .......... .......... .......... .......... .......... 35% 20.5M 10s
95650K .......... .......... .......... .......... .......... 36% 14.7M 10s
95700K .......... .......... .......... .......... .......... 36% 6.98M 10s
95750K .......... .......... .......... .......... .......... 36% 9.81M 10s
95800K .......... .......... .......... .......... .......... 36% 12.3M 10s
95850K .......... .......... .......... .......... .......... 36% 12.4M 10s
95900K .......... .......... .......... .......... .......... 36% 13.4M 10s
95950K .......... .......... .......... .......... .......... 36% 19.2M 10s
96000K .......... .......... .......... .......... .......... 36% 10.8M 10s
96050K .......... .......... .......... .......... .......... 36% 11.4M 10s
96100K .......... .......... .......... .......... .......... 36% 17.1M 10s
96150K .......... .......... .......... .......... .......... 36% 14.0M 10s
96200K .......... .......... .......... .......... .......... 36% 11.9M 10s
96250K .......... .......... .......... .......... .......... 36% 13.7M 10s
96300K .......... .......... .......... .......... .......... 36% 16.1M 10s
96350K .......... .......... .......... .......... .......... 36% 9.11M 10s
96400K .......... .......... .......... .......... .......... 36% 9.44M 10s
96450K .......... .......... .......... .......... .......... 36% 8.36M 10s
96500K .......... .......... .......... .......... .......... 36% 15.3M 10s
96550K .......... .......... .......... .......... .......... 36% 9.08M 10s
96600K .......... .......... .......... .......... .......... 36% 8.77M 10s
96650K .......... .......... .......... .......... .......... 36% 13.0M 10s
96700K .......... .......... .......... .......... .......... 36% 10.2M 10s
96750K .......... .......... .......... .......... .......... 36% 6.94M 10s
96800K .......... .......... .......... .......... .......... 36% 9.79M 10s
96850K .......... .......... .......... .......... .......... 36% 12.6M 10s
96900K .......... .......... .......... .......... .......... 36% 11.6M 10s
96950K .......... .......... .......... .......... .......... 36% 6.63M 10s
97000K .......... .......... .......... .......... .......... 36% 15.1M 10s
97050K .......... .......... .......... .......... .......... 36% 25.1M 10s
97100K .......... .......... .......... .......... .......... 36% 6.08M 10s
97150K .......... .......... .......... .......... .......... 36% 9.65M 10s
97200K .......... .......... .......... .......... .......... 36% 11.0M 10s
97250K .......... .......... .......... .......... .......... 36% 8.79M 10s
97300K .......... .......... .......... .......... .......... 36% 9.88M 10s
97350K .......... .......... .......... .......... .......... 36% 21.7M 10s
97400K .......... .......... .......... .......... .......... 36% 21.9M 10s
97450K .......... .......... .......... .......... .......... 36% 6.04M 10s
97500K .......... .......... .......... .......... .......... 36% 17.5M 10s
97550K .......... .......... .......... .......... .......... 36% 14.3M 10s
97600K .......... .......... .......... .......... .......... 36% 13.8M 10s
97650K .......... .......... .......... .......... .......... 36% 8.64M 10s
97700K .......... .......... .......... .......... .......... 36% 18.6M 10s
97750K .......... .......... .......... .......... .......... 36% 20.2M 10s
97800K .......... .......... .......... .......... .......... 36% 8.74M 10s
97850K .......... .......... .......... .......... .......... 36% 8.35M 10s
97900K .......... .......... .......... .......... .......... 36% 21.8M 10s
97950K .......... .......... .......... .......... .......... 36% 13.3M 10s
98000K .......... .......... .......... .......... .......... 36% 9.97M 10s
98050K .......... .......... .......... .......... .......... 36% 15.2M 10s
98100K .......... .......... .......... .......... .......... 36% 14.7M 10s
98150K .......... .......... .......... .......... .......... 36% 11.4M 10s
98200K .......... .......... .......... .......... .......... 36% 7.94M 10s
98250K .......... .......... .......... .......... .......... 36% 15.5M 10s
98300K .......... .......... .......... .......... .......... 37% 29.5M 10s
98350K .......... .......... .......... .......... .......... 37% 8.59M 10s
98400K .......... .......... .......... .......... .......... 37% 12.8M 10s
98450K .......... .......... .......... .......... .......... 37% 23.0M 10s
98500K .......... .......... .......... .......... .......... 37% 9.08M 10s
98550K .......... .......... .......... .......... .......... 37% 9.38M 10s
98600K .......... .......... .......... .......... .......... 37% 13.5M 10s
98650K .......... .......... .......... .......... .......... 37% 20.6M 10s
98700K .......... .......... .......... .......... .......... 37% 8.27M 10s
98750K .......... .......... .......... .......... .......... 37% 14.4M 10s
98800K .......... .......... .......... .......... .......... 37% 15.1M 10s
98850K .......... .......... .......... .......... .......... 37% 10.2M 10s
98900K .......... .......... .......... .......... .......... 37% 9.53M 10s
98950K .......... .......... .......... .......... .......... 37% 12.2M 10s
99000K .......... .......... .......... .......... .......... 37% 46.4M 10s
99050K .......... .......... .......... .......... .......... 37% 9.22M 10s
99100K .......... .......... .......... .......... .......... 37% 9.12M 10s
99150K .......... .......... .......... .......... .......... 37% 18.4M 10s
99200K .......... .......... .......... .......... .......... 37% 9.38M 10s
99250K .......... .......... .......... .......... .......... 37% 12.1M 10s
99300K .......... .......... .......... .......... .......... 37% 11.3M 10s
99350K .......... .......... .......... .......... .......... 37% 26.6M 10s
99400K .......... .......... .......... .......... .......... 37% 8.70M 10s
99450K .......... .......... .......... .......... .......... 37% 9.79M 10s
99500K .......... .......... .......... .......... .......... 37% 16.7M 10s
99550K .......... .......... .......... .......... .......... 37% 15.0M 10s
99600K .......... .......... .......... .......... .......... 37% 7.64M 10s
99650K .......... .......... .......... .......... .......... 37% 15.6M 10s
99700K .......... .......... .......... .......... .......... 37% 18.7M 10s
99750K .......... .......... .......... .......... .......... 37% 8.68M 10s
99800K .......... .......... .......... .......... .......... 37% 10.7M 10s
99850K .......... .......... .......... .......... .......... 37% 12.9M 10s
99900K .......... .......... .......... .......... .......... 37% 22.2M 10s
99950K .......... .......... .......... .......... .......... 37% 7.22M 10s
100000K .......... .......... .......... .......... .......... 37% 16.3M 10s
100050K .......... .......... .......... .......... .......... 37% 14.1M 10s
100100K .......... .......... .......... .......... .......... 37% 19.4M 10s
100150K .......... .......... .......... .......... .......... 37% 7.63M 10s
100200K .......... .......... .......... .......... .......... 37% 10.8M 10s
100250K .......... .......... .......... .......... .......... 37% 19.6M 10s
100300K .......... .......... .......... .......... .......... 37% 13.3M 10s
100350K .......... .......... .......... .......... .......... 37% 7.59M 10s
100400K .......... .......... .......... .......... .......... 37% 17.9M 10s
100450K .......... .......... .......... .......... .......... 37% 20.3M 10s
100500K .......... .......... .......... .......... .......... 37% 10.8M 10s
100550K .......... .......... .......... .......... .......... 37% 9.23M 10s
100600K .......... .......... .......... .......... .......... 37% 12.4M 10s
100650K .......... .......... .......... .......... .......... 37% 18.8M 10s
100700K .......... .......... .......... .......... .......... 37% 8.43M 10s
100750K .......... .......... .......... .......... .......... 37% 14.0M 10s
100800K .......... .......... .......... .......... .......... 37% 22.9M 10s
100850K .......... .......... .......... .......... .......... 37% 9.33M 10s
100900K .......... .......... .......... .......... .......... 37% 11.4M 10s
100950K .......... .......... .......... .......... .......... 38% 11.0M 10s
101000K .......... .......... .......... .......... .......... 38% 16.6M 10s
101050K .......... .......... .......... .......... .......... 38% 12.0M 10s
101100K .......... .......... .......... .......... .......... 38% 12.7M 10s
101150K .......... .......... .......... .......... .......... 38% 10.7M 10s
101200K .......... .......... .......... .......... .......... 38% 17.0M 10s
101250K .......... .......... .......... .......... .......... 38% 7.86M 10s
101300K .......... .......... .......... .......... .......... 38% 15.6M 10s
101350K .......... .......... .......... .......... .......... 38% 16.0M 10s
101400K .......... .......... .......... .......... .......... 38% 11.5M 10s
101450K .......... .......... .......... .......... .......... 38% 8.79M 10s
101500K .......... .......... .......... .......... .......... 38% 17.2M 10s
101550K .......... .......... .......... .......... .......... 38% 15.2M 10s
101600K .......... .......... .......... .......... .......... 38% 13.2M 10s
101650K .......... .......... .......... .......... .......... 38% 8.71M 10s
101700K .......... .......... .......... .......... .......... 38% 13.1M 10s
101750K .......... .......... .......... .......... .......... 38% 24.0M 9s
101800K .......... .......... .......... .......... .......... 38% 13.2M 9s
101850K .......... .......... .......... .......... .......... 38% 8.14M 10s
101900K .......... .......... .......... .......... .......... 38% 13.1M 9s
101950K .......... .......... .......... .......... .......... 38% 12.6M 9s
102000K .......... .......... .......... .......... .......... 38% 7.71M 9s
102050K .......... .......... .......... .......... .......... 38% 28.8M 9s
102100K .......... .......... .......... .......... .......... 38% 8.14M 9s
102150K .......... .......... .......... .......... .......... 38% 27.2M 9s
102200K .......... .......... .......... .......... .......... 38% 7.92M 9s
102250K .......... .......... .......... .......... .......... 38% 14.6M 9s
102300K .......... .......... .......... .......... .......... 38% 14.9M 9s
102350K .......... .......... .......... .......... .......... 38% 17.9M 9s
102400K .......... .......... .......... .......... .......... 38% 7.19M 9s
102450K .......... .......... .......... .......... .......... 38% 14.8M 9s
102500K .......... .......... .......... .......... .......... 38% 16.5M 9s
102550K .......... .......... .......... .......... .......... 38% 25.4M 9s
102600K .......... .......... .......... .......... .......... 38% 6.96M 9s
102650K .......... .......... .......... .......... .......... 38% 15.4M 9s
102700K .......... .......... .......... .......... .......... 38% 11.3M 9s
102750K .......... .......... .......... .......... .......... 38% 36.6M 9s
102800K .......... .......... .......... .......... .......... 38% 6.40M 9s
102850K .......... .......... .......... .......... .......... 38% 15.9M 9s
102900K .......... .......... .......... .......... .......... 38% 13.6M 9s
102950K .......... .......... .......... .......... .......... 38% 15.4M 9s
103000K .......... .......... .......... .......... .......... 38% 7.58M 9s
103050K .......... .......... .......... .......... .......... 38% 13.9M 9s
103100K .......... .......... .......... .......... .......... 38% 13.8M 9s
103150K .......... .......... .......... .......... .......... 38% 10.3M 9s
103200K .......... .......... .......... .......... .......... 38% 8.12M 9s
103250K .......... .......... .......... .......... .......... 38% 27.7M 9s
103300K .......... .......... .......... .......... .......... 38% 13.6M 9s
103350K .......... .......... .......... .......... .......... 38% 6.85M 9s
103400K .......... .......... .......... .......... .......... 38% 14.0M 9s
103450K .......... .......... .......... .......... .......... 38% 13.1M 9s
103500K .......... .......... .......... .......... .......... 38% 20.9M 9s
103550K .......... .......... .......... .......... .......... 38% 7.72M 9s
103600K .......... .......... .......... .......... .......... 39% 13.7M 9s
103650K .......... .......... .......... .......... .......... 39% 15.1M 9s
103700K .......... .......... .......... .......... .......... 39% 11.9M 9s
103750K .......... .......... .......... .......... .......... 39% 8.54M 9s
103800K .......... .......... .......... .......... .......... 39% 18.2M 9s
103850K .......... .......... .......... .......... .......... 39% 14.2M 9s
103900K .......... .......... .......... .......... .......... 39% 11.8M 9s
103950K .......... .......... .......... .......... .......... 39% 8.71M 9s
104000K .......... .......... .......... .......... .......... 39% 15.5M 9s
104050K .......... .......... .......... .......... .......... 39% 13.8M 9s
104100K .......... .......... .......... .......... .......... 39% 12.7M 9s
104150K .......... .......... .......... .......... .......... 39% 8.59M 9s
104200K .......... .......... .......... .......... .......... 39% 11.9M 9s
104250K .......... .......... .......... .......... .......... 39% 32.8M 9s
104300K .......... .......... .......... .......... .......... 39% 9.67M 9s
104350K .......... .......... .......... .......... .......... 39% 8.54M 9s
104400K .......... .......... .......... .......... .......... 39% 14.8M 9s
104450K .......... .......... .......... .......... .......... 39% 17.8M 9s
104500K .......... .......... .......... .......... .......... 39% 11.1M 9s
104550K .......... .......... .......... .......... .......... 39% 8.40M 9s
104600K .......... .......... .......... .......... .......... 39% 14.7M 9s
104650K .......... .......... .......... .......... .......... 39% 19.7M 9s
104700K .......... .......... .......... .......... .......... 39% 10.3M 9s
104750K .......... .......... .......... .......... .......... 39% 8.57M 9s
104800K .......... .......... .......... .......... .......... 39% 14.2M 9s
104850K .......... .......... .......... .......... .......... 39% 19.1M 9s
104900K .......... .......... .......... .......... .......... 39% 10.9M 9s
104950K .......... .......... .......... .......... .......... 39% 7.82M 9s
105000K .......... .......... .......... .......... .......... 39% 15.0M 9s
105050K .......... .......... .......... .......... .......... 39% 23.7M 9s
105100K .......... .......... .......... .......... .......... 39% 11.5M 9s
105150K .......... .......... .......... .......... .......... 39% 8.66M 9s
105200K .......... .......... .......... .......... .......... 39% 11.0M 9s
105250K .......... .......... .......... .......... .......... 39% 16.6M 9s
105300K .......... .......... .......... .......... .......... 39% 22.3M 9s
105350K .......... .......... .......... .......... .......... 39% 6.73M 9s
105400K .......... .......... .......... .......... .......... 39% 14.3M 9s
105450K .......... .......... .......... .......... .......... 39% 14.2M 9s
105500K .......... .......... .......... .......... .......... 39% 20.2M 9s
105550K .......... .......... .......... .......... .......... 39% 6.98M 9s
105600K .......... .......... .......... .......... .......... 39% 13.4M 9s
105650K .......... .......... .......... .......... .......... 39% 14.8M 9s
105700K .......... .......... .......... .......... .......... 39% 16.7M 9s
105750K .......... .......... .......... .......... .......... 39% 7.55M 9s
105800K .......... .......... .......... .......... .......... 39% 17.7M 9s
105850K .......... .......... .......... .......... .......... 39% 11.2M 9s
105900K .......... .......... .......... .......... .......... 39% 23.8M 9s
105950K .......... .......... .......... .......... .......... 39% 6.40M 9s
106000K .......... .......... .......... .......... .......... 39% 17.2M 9s
106050K .......... .......... .......... .......... .......... 39% 19.0M 9s
106100K .......... .......... .......... .......... .......... 39% 12.8M 9s
106150K .......... .......... .......... .......... .......... 39% 7.61M 9s
106200K .......... .......... .......... .......... .......... 39% 12.2M 9s
106250K .......... .......... .......... .......... .......... 40% 20.0M 9s
106300K .......... .......... .......... .......... .......... 40% 14.8M 9s
106350K .......... .......... .......... .......... .......... 40% 7.86M 9s
106400K .......... .......... .......... .......... .......... 40% 15.9M 9s
106450K .......... .......... .......... .......... .......... 40% 9.44M 9s
106500K .......... .......... .......... .......... .......... 40% 19.8M 9s
106550K .......... .......... .......... .......... .......... 40% 25.4M 9s
106600K .......... .......... .......... .......... .......... 40% 6.25M 9s
106650K .......... .......... .......... .......... .......... 40% 13.6M 9s
106700K .......... .......... .......... .......... .......... 40% 13.0M 9s
106750K .......... .......... .......... .......... .......... 40% 28.7M 9s
106800K .......... .......... .......... .......... .......... 40% 6.72M 9s
106850K .......... .......... .......... .......... .......... 40% 11.4M 9s
106900K .......... .......... .......... .......... .......... 40% 21.6M 9s
106950K .......... .......... .......... .......... .......... 40% 14.2M 9s
107000K .......... .......... .......... .......... .......... 40% 7.45M 9s
107050K .......... .......... .......... .......... .......... 40% 12.3M 9s
107100K .......... .......... .......... .......... .......... 40% 14.5M 9s
107150K .......... .......... .......... .......... .......... 40% 19.8M 9s
107200K .......... .......... .......... .......... .......... 40% 6.52M 9s
107250K .......... .......... .......... .......... .......... 40% 19.9M 9s
107300K .......... .......... .......... .......... .......... 40% 10.6M 9s
107350K .......... .......... .......... .......... .......... 40% 19.9M 9s
107400K .......... .......... .......... .......... .......... 40% 9.68M 9s
107450K .......... .......... .......... .......... .......... 40% 10.4M 9s
107500K .......... .......... .......... .......... .......... 40% 10.2M 9s
107550K .......... .......... .......... .......... .......... 40% 27.6M 9s
107600K .......... .......... .......... .......... .......... 40% 8.35M 9s
107650K .......... .......... .......... .......... .......... 40% 11.6M 9s
107700K .......... .......... .......... .......... .......... 40% 10.1M 9s
107750K .......... .......... .......... .......... .......... 40% 23.9M 9s
107800K .......... .......... .......... .......... .......... 40% 17.7M 9s
107850K .......... .......... .......... .......... .......... 40% 7.07M 9s
107900K .......... .......... .......... .......... .......... 40% 12.6M 9s
107950K .......... .......... .......... .......... .......... 40% 12.8M 9s
108000K .......... .......... .......... .......... .......... 40% 23.0M 9s
108050K .......... .......... .......... .......... .......... 40% 9.25M 9s
108100K .......... .......... .......... .......... .......... 40% 8.77M 9s
108150K .......... .......... .......... .......... .......... 40% 12.2M 9s
108200K .......... .......... .......... .......... .......... 40% 25.3M 9s
108250K .......... .......... .......... .......... .......... 40% 9.35M 9s
108300K .......... .......... .......... .......... .......... 40% 11.0M 9s
108350K .......... .......... .......... .......... .......... 40% 7.61M 9s
108400K .......... .......... .......... .......... .......... 40% 15.8M 9s
108450K .......... .......... .......... .......... .......... 40% 13.9M 9s
108500K .......... .......... .......... .......... .......... 40% 10.9M 9s
108550K .......... .......... .......... .......... .......... 40% 17.8M 9s
108600K .......... .......... .......... .......... .......... 40% 12.3M 9s
108650K .......... .......... .......... .......... .......... 40% 18.7M 9s
108700K .......... .......... .......... .......... .......... 40% 7.06M 9s
108750K .......... .......... .......... .......... .......... 40% 12.8M 9s
108800K .......... .......... .......... .......... .......... 40% 14.7M 9s
108850K .......... .......... .......... .......... .......... 40% 24.8M 9s
108900K .......... .......... .......... .......... .......... 40% 8.52M 9s
108950K .......... .......... .......... .......... .......... 41% 7.62M 9s
109000K .......... .......... .......... .......... .......... 41% 16.1M 9s
109050K .......... .......... .......... .......... .......... 41% 19.7M 9s
109100K .......... .......... .......... .......... .......... 41% 16.4M 9s
109150K .......... .......... .......... .......... .......... 41% 6.83M 9s
109200K .......... .......... .......... .......... .......... 41% 11.0M 9s
109250K .......... .......... .......... .......... .......... 41% 31.0M 9s
109300K .......... .......... .......... .......... .......... 41% 15.0M 9s
109350K .......... .......... .......... .......... .......... 41% 7.68M 9s
109400K .......... .......... .......... .......... .......... 41% 10.9M 9s
109450K .......... .......... .......... .......... .......... 41% 11.8M 9s
109500K .......... .......... .......... .......... .......... 41% 27.6M 9s
109550K .......... .......... .......... .......... .......... 41% 9.00M 9s
109600K .......... .......... .......... .......... .......... 41% 7.36M 9s
109650K .......... .......... .......... .......... .......... 41% 17.4M 9s
109700K .......... .......... .......... .......... .......... 41% 20.3M 9s
109750K .......... .......... .......... .......... .......... 41% 15.0M 9s
109800K .......... .......... .......... .......... .......... 41% 7.43M 9s
109850K .......... .......... .......... .......... .......... 41% 19.1M 9s
109900K .......... .......... .......... .......... .......... 41% 12.7M 9s
109950K .......... .......... .......... .......... .......... 41% 14.4M 9s
110000K .......... .......... .......... .......... .......... 41% 7.76M 9s
110050K .......... .......... .......... .......... .......... 41% 13.7M 9s
110100K .......... .......... .......... .......... .......... 41% 12.0M 9s
110150K .......... .......... .......... .......... .......... 41% 30.0M 9s
110200K .......... .......... .......... .......... .......... 41% 11.0M 9s
110250K .......... .......... .......... .......... .......... 41% 7.45M 9s
110300K .......... .......... .......... .......... .......... 41% 11.8M 9s
110350K .......... .......... .......... .......... .......... 41% 28.8M 9s
110400K .......... .......... .......... .......... .......... 41% 12.7M 9s
110450K .......... .......... .......... .......... .......... 41% 8.62M 9s
110500K .......... .......... .......... .......... .......... 41% 10.3M 9s
110550K .......... .......... .......... .......... .......... 41% 17.9M 9s
110600K .......... .......... .......... .......... .......... 41% 16.8M 9s
110650K .......... .......... .......... .......... .......... 41% 14.5M 9s
110700K .......... .......... .......... .......... .......... 41% 5.87M 9s
110750K .......... .......... .......... .......... .......... 41% 18.4M 9s
110800K .......... .......... .......... .......... .......... 41% 34.8M 9s
110850K .......... .......... .......... .......... .......... 41% 11.3M 9s
110900K .......... .......... .......... .......... .......... 41% 8.94M 9s
110950K .......... .......... .......... .......... .......... 41% 11.9M 9s
111000K .......... .......... .......... .......... .......... 41% 14.2M 9s
111050K .......... .......... .......... .......... .......... 41% 23.5M 9s
111100K .......... .......... .......... .......... .......... 41% 7.58M 9s
111150K .......... .......... .......... .......... .......... 41% 12.2M 9s
111200K .......... .......... .......... .......... .......... 41% 12.4M 9s
111250K .......... .......... .......... .......... .......... 41% 21.4M 9s
111300K .......... .......... .......... .......... .......... 41% 11.8M 9s
111350K .......... .......... .......... .......... .......... 41% 9.10M 9s
111400K .......... .......... .......... .......... .......... 41% 12.0M 9s
111450K .......... .......... .......... .......... .......... 41% 15.9M 9s
111500K .......... .......... .......... .......... .......... 41% 17.4M 9s
111550K .......... .......... .......... .......... .......... 41% 7.90M 9s
111600K .......... .......... .......... .......... .......... 42% 12.2M 9s
111650K .......... .......... .......... .......... .......... 42% 11.9M 9s
111700K .......... .......... .......... .......... .......... 42% 14.6M 9s
111750K .......... .......... .......... .......... .......... 42% 18.0M 9s
111800K .......... .......... .......... .......... .......... 42% 9.04M 9s
111850K .......... .......... .......... .......... .......... 42% 9.09M 9s
111900K .......... .......... .......... .......... .......... 42% 23.7M 9s
111950K .......... .......... .......... .......... .......... 42% 17.7M 9s
112000K .......... .......... .......... .......... .......... 42% 8.75M 9s
112050K .......... .......... .......... .......... .......... 42% 11.5M 9s
112100K .......... .......... .......... .......... .......... 42% 10.0M 9s
112150K .......... .......... .......... .......... .......... 42% 17.0M 9s
112200K .......... .......... .......... .......... .......... 42% 24.1M 9s
112250K .......... .......... .......... .......... .......... 42% 6.79M 9s
112300K .......... .......... .......... .......... .......... 42% 16.8M 9s
112350K .......... .......... .......... .......... .......... 42% 14.8M 9s
112400K .......... .......... .......... .......... .......... 42% 17.9M 9s
112450K .......... .......... .......... .......... .......... 42% 8.54M 9s
112500K .......... .......... .......... .......... .......... 42% 11.2M 9s
112550K .......... .......... .......... .......... .......... 42% 10.5M 9s
112600K .......... .......... .......... .......... .......... 42% 20.9M 9s
112650K .......... .......... .......... .......... .......... 42% 21.4M 9s
112700K .......... .......... .......... .......... .......... 42% 8.44M 9s
112750K .......... .......... .......... .......... .......... 42% 8.95M 9s
112800K .......... .......... .......... .......... .......... 42% 15.9M 9s
112850K .......... .......... .......... .......... .......... 42% 15.2M 9s
112900K .......... .......... .......... .......... .......... 42% 16.3M 9s
112950K .......... .......... .......... .......... .......... 42% 7.14M 9s
113000K .......... .......... .......... .......... .......... 42% 10.9M 9s
113050K .......... .......... .......... .......... .......... 42% 35.8M 9s
113100K .......... .......... .......... .......... .......... 42% 13.5M 9s
113150K .......... .......... .......... .......... .......... 42% 10.1M 9s
113200K .......... .......... .......... .......... .......... 42% 7.85M 9s
113250K .......... .......... .......... .......... .......... 42% 16.1M 9s
113300K .......... .......... .......... .......... .......... 42% 15.6M 9s
113350K .......... .......... .......... .......... .......... 42% 25.0M 9s
113400K .......... .......... .......... .......... .......... 42% 7.61M 9s
113450K .......... .......... .......... .......... .......... 42% 10.3M 9s
113500K .......... .......... .......... .......... .......... 42% 16.9M 9s
113550K .......... .......... .......... .......... .......... 42% 14.2M 9s
113600K .......... .......... .......... .......... .......... 42% 10.4M 9s
113650K .......... .......... .......... .......... .......... 42% 8.32M 9s
113700K .......... .......... .......... .......... .......... 42% 13.9M 9s
113750K .......... .......... .......... .......... .......... 42% 15.7M 9s
113800K .......... .......... .......... .......... .......... 42% 24.9M 9s
113850K .......... .......... .......... .......... .......... 42% 7.29M 9s
113900K .......... .......... .......... .......... .......... 42% 13.9M 9s
113950K .......... .......... .......... .......... .......... 42% 12.3M 9s
114000K .......... .......... .......... .......... .......... 42% 19.4M 9s
114050K .......... .......... .......... .......... .......... 42% 17.8M 9s
114100K .......... .......... .......... .......... .......... 42% 5.95M 9s
114150K .......... .......... .......... .......... .......... 42% 15.9M 9s
114200K .......... .......... .......... .......... .......... 42% 17.9M 9s
114250K .......... .......... .......... .......... .......... 43% 17.5M 9s
114300K .......... .......... .......... .......... .......... 43% 9.88M 9s
114350K .......... .......... .......... .......... .......... 43% 9.21M 9s
114400K .......... .......... .......... .......... .......... 43% 16.1M 9s
114450K .......... .......... .......... .......... .......... 43% 12.9M 9s
114500K .......... .......... .......... .......... .......... 43% 26.9M 9s
114550K .......... .......... .......... .......... .......... 43% 8.64M 9s
114600K .......... .......... .......... .......... .......... 43% 11.2M 9s
114650K .......... .......... .......... .......... .......... 43% 9.97M 9s
114700K .......... .......... .......... .......... .......... 43% 22.6M 9s
114750K .......... .......... .......... .......... .......... 43% 13.9M 9s
114800K .......... .......... .......... .......... .......... 43% 9.03M 9s
114850K .......... .......... .......... .......... .......... 43% 9.81M 9s
114900K .......... .......... .......... .......... .......... 43% 7.49M 9s
114950K .......... .......... .......... .......... .......... 43% 52.4M 9s
115000K .......... .......... .......... .......... .......... 43% 15.7M 9s
115050K .......... .......... .......... .......... .......... 43% 9.69M 9s
115100K .......... .......... .......... .......... .......... 43% 12.8M 9s
115150K .......... .......... .......... .......... .......... 43% 13.6M 9s
115200K .......... .......... .......... .......... .......... 43% 17.9M 9s
115250K .......... .......... .......... .......... .......... 43% 12.8M 9s
115300K .......... .......... .......... .......... .......... 43% 9.67M 9s
115350K .......... .......... .......... .......... .......... 43% 14.8M 9s
115400K .......... .......... .......... .......... .......... 43% 3.71M 9s
115450K .......... .......... .......... .......... .......... 43% 93.0M 9s
115500K .......... .......... .......... .......... .......... 43% 102M 9s
115550K .......... .......... .......... .......... .......... 43% 27.2M 9s
115600K .......... .......... .......... .......... .......... 43% 9.43M 9s
115650K .......... .......... .......... .......... .......... 43% 23.2M 9s
115700K .......... .......... .......... .......... .......... 43% 5.92M 9s
115750K .......... .......... .......... .......... .......... 43% 20.6M 9s
115800K .......... .......... .......... .......... .......... 43% 17.5M 9s
115850K .......... .......... .......... .......... .......... 43% 10.6M 9s
115900K .......... .......... .......... .......... .......... 43% 6.05M 9s
115950K .......... .......... .......... .......... .......... 43% 36.1M 9s
116000K .......... .......... .......... .......... .......... 43% 23.7M 9s
116050K .......... .......... .......... .......... .......... 43% 14.0M 9s
116100K .......... .......... .......... .......... .......... 43% 11.7M 9s
116150K .......... .......... .......... .......... .......... 43% 5.96M 9s
116200K .......... .......... .......... .......... .......... 43% 22.4M 9s
116250K .......... .......... .......... .......... .......... 43% 27.1M 9s
116300K .......... .......... .......... .......... .......... 43% 20.0M 9s
116350K .......... .......... .......... .......... .......... 43% 8.57M 9s
116400K .......... .......... .......... .......... .......... 43% 6.45M 9s
116450K .......... .......... .......... .......... .......... 43% 27.7M 9s
116500K .......... .......... .......... .......... .......... 43% 23.2M 9s
116550K .......... .......... .......... .......... .......... 43% 23.6M 9s
116600K .......... .......... .......... .......... .......... 43% 3.99M 9s
116650K .......... .......... .......... .......... .......... 43% 32.5M 9s
116700K .......... .......... .......... .......... .......... 43% 21.6M 9s
116750K .......... .......... .......... .......... .......... 43% 34.2M 9s
116800K .......... .......... .......... .......... .......... 43% 16.4M 9s
116850K .......... .......... .......... .......... .......... 43% 4.46M 9s
116900K .......... .......... .......... .......... .......... 44% 22.8M 9s
116950K .......... .......... .......... .......... .......... 44% 22.9M 9s
117000K .......... .......... .......... .......... .......... 44% 18.2M 9s
117050K .......... .......... .......... .......... .......... 44% 16.9M 9s
117100K .......... .......... .......... .......... .......... 44% 4.89M 9s
117150K .......... .......... .......... .......... .......... 44% 24.2M 9s
117200K .......... .......... .......... .......... .......... 44% 23.1M 9s
117250K .......... .......... .......... .......... .......... 44% 17.5M 9s
117300K .......... .......... .......... .......... .......... 44% 14.5M 9s
117350K .......... .......... .......... .......... .......... 44% 5.15M 9s
117400K .......... .......... .......... .......... .......... 44% 25.3M 9s
117450K .......... .......... .......... .......... .......... 44% 20.0M 9s
117500K .......... .......... .......... .......... .......... 44% 26.1M 9s
117550K .......... .......... .......... .......... .......... 44% 14.8M 9s
117600K .......... .......... .......... .......... .......... 44% 4.97M 9s
117650K .......... .......... .......... .......... .......... 44% 26.6M 9s
117700K .......... .......... .......... .......... .......... 44% 23.8M 9s
117750K .......... .......... .......... .......... .......... 44% 16.8M 9s
117800K .......... .......... .......... .......... .......... 44% 11.0M 9s
117850K .......... .......... .......... .......... .......... 44% 6.21M 9s
117900K .......... .......... .......... .......... .......... 44% 26.0M 9s
117950K .......... .......... .......... .......... .......... 44% 28.2M 9s
118000K .......... .......... .......... .......... .......... 44% 2.02M 9s
118050K .......... .......... .......... .......... .......... 44% 18.9M 9s
118100K .......... .......... .......... .......... .......... 44% 67.7M 9s
118150K .......... .......... .......... .......... .......... 44% 90.0M 9s
118200K .......... .......... .......... .......... .......... 44% 79.8M 9s
118250K .......... .......... .......... .......... .......... 44% 102M 9s
118300K .......... .......... .......... .......... .......... 44% 13.9M 9s
118350K .......... .......... .......... .......... .......... 44% 12.9M 9s
118400K .......... .......... .......... .......... .......... 44% 15.0M 9s
118450K .......... .......... .......... .......... .......... 44% 6.79M 9s
118500K .......... .......... .......... .......... .......... 44% 8.93M 9s
118550K .......... .......... .......... .......... .......... 44% 21.1M 9s
118600K .......... .......... .......... .......... .......... 44% 9.47M 9s
118650K .......... .......... .......... .......... .......... 44% 6.95M 9s
118700K .......... .......... .......... .......... .......... 44% 25.8M 9s
118750K .......... .......... .......... .......... .......... 44% 20.4M 9s
118800K .......... .......... .......... .......... .......... 44% 8.69M 9s
118850K .......... .......... .......... .......... .......... 44% 6.62M 9s
118900K .......... .......... .......... .......... .......... 44% 24.1M 9s
118950K .......... .......... .......... .......... .......... 44% 7.68M 9s
119000K .......... .......... .......... .......... .......... 44% 7.75M 9s
119050K .......... .......... .......... .......... .......... 44% 36.7M 9s
119100K .......... .......... .......... .......... .......... 44% 8.71M 9s
119150K .......... .......... .......... .......... .......... 44% 20.1M 9s
119200K .......... .......... .......... .......... .......... 44% 6.61M 9s
119250K .......... .......... .......... .......... .......... 44% 18.4M 9s
119300K .......... .......... .......... .......... .......... 44% 13.0M 9s
119350K .......... .......... .......... .......... .......... 44% 5.74M 9s
119400K .......... .......... .......... .......... .......... 44% 31.7M 9s
119450K .......... .......... .......... .......... .......... 44% 9.03M 9s
119500K .......... .......... .......... .......... .......... 44% 18.1M 9s
119550K .......... .......... .......... .......... .......... 45% 7.01M 9s
119600K .......... .......... .......... .......... .......... 45% 15.2M 9s
119650K .......... .......... .......... .......... .......... 45% 13.7M 9s
119700K .......... .......... .......... .......... .......... 45% 5.61M 9s
119750K .......... .......... .......... .......... .......... 45% 24.6M 9s
119800K .......... .......... .......... .......... .......... 45% 21.1M 9s
119850K .......... .......... .......... .......... .......... 45% 5.07M 9s
119900K .......... .......... .......... .......... .......... 45% 13.3M 9s
119950K .......... .......... .......... .......... .......... 45% 27.7M 9s
120000K .......... .......... .......... .......... .......... 45% 12.8M 9s
120050K .......... .......... .......... .......... .......... 45% 5.55M 9s
120100K .......... .......... .......... .......... .......... 45% 25.2M 9s
120150K .......... .......... .......... .......... .......... 45% 19.8M 9s
120200K .......... .......... .......... .......... .......... 45% 8.72M 9s
120250K .......... .......... .......... .......... .......... 45% 6.04M 9s
120300K .......... .......... .......... .......... .......... 45% 53.1M 9s
120350K .......... .......... .......... .......... .......... 45% 11.6M 9s
120400K .......... .......... .......... .......... .......... 45% 5.54M 9s
120450K .......... .......... .......... .......... .......... 45% 18.1M 9s
120500K .......... .......... .......... .......... .......... 45% 32.9M 9s
120550K .......... .......... .......... .......... .......... 45% 8.27M 9s
120600K .......... .......... .......... .......... .......... 45% 7.05M 9s
120650K .......... .......... .......... .......... .......... 45% 21.2M 9s
120700K .......... .......... .......... .......... .......... 45% 11.5M 9s
120750K .......... .......... .......... .......... .......... 45% 6.86M 9s
120800K .......... .......... .......... .......... .......... 45% 13.2M 9s
120850K .......... .......... .......... .......... .......... 45% 19.7M 9s
120900K .......... .......... .......... .......... .......... 45% 11.2M 9s
120950K .......... .......... .......... .......... .......... 45% 5.53M 9s
121000K .......... .......... .......... .......... .......... 45% 21.5M 9s
121050K .......... .......... .......... .......... .......... 45% 24.3M 9s
121100K .......... .......... .......... .......... .......... 45% 6.12M 9s
121150K .......... .......... .......... .......... .......... 45% 5.10M 9s
121200K .......... .......... .......... .......... .......... 45% 12.7M 9s
121250K .......... .......... .......... .......... .......... 45% 1.83M 9s
121300K .......... .......... .......... .......... .......... 45% 73.9M 9s
121350K .......... .......... .......... .......... .......... 45% 73.2M 9s
121400K .......... .......... .......... .......... .......... 45% 5.00M 9s
121450K .......... .......... .......... .......... .......... 45% 67.4M 9s
121500K .......... .......... .......... .......... .......... 45% 135M 9s
121550K .......... .......... .......... .......... .......... 45% 10.8M 9s
121600K .......... .......... .......... .......... .......... 45% 5.95M 9s
121650K .......... .......... .......... .......... .......... 45% 9.43M 9s
121700K .......... .......... .......... .......... .......... 45% 5.35M 9s
121750K .......... .......... .......... .......... .......... 45% 12.9M 9s
121800K .......... .......... .......... .......... .......... 45% 8.33M 9s
121850K .......... .......... .......... .......... .......... 45% 5.41M 9s
121900K .......... .......... .......... .......... .......... 45% 11.2M 9s
121950K .......... .......... .......... .......... .......... 45% 6.27M 9s
122000K .......... .......... .......... .......... .......... 45% 16.1M 9s
122050K .......... .......... .......... .......... .......... 45% 15.2M 9s
122100K .......... .......... .......... .......... .......... 45% 5.48M 9s
122150K .......... .......... .......... .......... .......... 45% 45.6M 9s
122200K .......... .......... .......... .......... .......... 46% 5.75M 9s
122250K .......... .......... .......... .......... .......... 46% 13.7M 9s
122300K .......... .......... .......... .......... .......... 46% 15.8M 9s
122350K .......... .......... .......... .......... .......... 46% 6.04M 9s
122400K .......... .......... .......... .......... .......... 46% 21.8M 9s
122450K .......... .......... .......... .......... .......... 46% 5.96M 9s
122500K .......... .......... .......... .......... .......... 46% 17.4M 9s
122550K .......... .......... .......... .......... .......... 46% 11.5M 9s
122600K .......... .......... .......... .......... .......... 46% 6.43M 9s
122650K .......... .......... .......... .......... .......... 46% 26.5M 9s
122700K .......... .......... .......... .......... .......... 46% 5.48M 9s
122750K .......... .......... .......... .......... .......... 46% 12.9M 9s
122800K .......... .......... .......... .......... .......... 46% 13.3M 9s
122850K .......... .......... .......... .......... .......... 46% 7.09M 9s
122900K .......... .......... .......... .......... .......... 46% 18.1M 9s
122950K .......... .......... .......... .......... .......... 46% 9.53M 9s
123000K .......... .......... .......... .......... .......... 46% 7.80M 9s
123050K .......... .......... .......... .......... .......... 46% 16.1M 9s
123100K .......... .......... .......... .......... .......... 46% 6.65M 9s
123150K .......... .......... .......... .......... .......... 46% 12.6M 9s
123200K .......... .......... .......... .......... .......... 46% 10.0M 9s
123250K .......... .......... .......... .......... .......... 46% 8.12M 9s
123300K .......... .......... .......... .......... .......... 46% 20.4M 9s
123350K .......... .......... .......... .......... .......... 46% 5.75M 9s
123400K .......... .......... .......... .......... .......... 46% 13.5M 9s
123450K .......... .......... .......... .......... .......... 46% 7.51M 9s
123500K .......... .......... .......... .......... .......... 46% 9.37M 9s
123550K .......... .......... .......... .......... .......... 46% 21.0M 9s
123600K .......... .......... .......... .......... .......... 46% 9.04M 9s
123650K .......... .......... .......... .......... .......... 46% 8.33M 9s
123700K .......... .......... .......... .......... .......... 46% 21.1M 9s
123750K .......... .......... .......... .......... .......... 46% 9.13M 9s
123800K .......... .......... .......... .......... .......... 46% 6.96M 9s
123850K .......... .......... .......... .......... .......... 46% 65.3M 9s
123900K .......... .......... .......... .......... .......... 46% 5.69M 9s
123950K .......... .......... .......... .......... .......... 46% 10.3M 9s
124000K .......... .......... .......... .......... .......... 46% 33.3M 9s
124050K .......... .......... .......... .......... .......... 46% 6.44M 9s
124100K .......... .......... .......... .......... .......... 46% 11.2M 9s
124150K .......... .......... .......... .......... .......... 46% 11.4M 9s
124200K .......... .......... .......... .......... .......... 46% 7.00M 9s
124250K .......... .......... .......... .......... .......... 46% 20.9M 9s
124300K .......... .......... .......... .......... .......... 46% 9.06M 9s
124350K .......... .......... .......... .......... .......... 46% 6.97M 9s
124400K .......... .......... .......... .......... .......... 46% 43.9M 9s
124450K .......... .......... .......... .......... .......... 46% 5.54M 9s
124500K .......... .......... .......... .......... .......... 46% 10.9M 9s
124550K .......... .......... .......... .......... .......... 46% 29.0M 9s
124600K .......... .......... .......... .......... .......... 46% 2.86M 9s
124650K .......... .......... .......... .......... .......... 46% 24.5M 9s
124700K .......... .......... .......... .......... .......... 46% 84.2M 9s
124750K .......... .......... .......... .......... .......... 46% 13.4M 9s
124800K .......... .......... .......... .......... .......... 46% 9.93M 9s
124850K .......... .......... .......... .......... .......... 47% 5.63M 9s
124900K .......... .......... .......... .......... .......... 47% 11.4M 9s
124950K .......... .......... .......... .......... .......... 47% 5.81M 9s
125000K .......... .......... .......... .......... .......... 47% 7.69M 9s
125050K .......... .......... .......... .......... .......... 47% 9.20M 9s
125100K .......... .......... .......... .......... .......... 47% 6.66M 9s
125150K .......... .......... .......... .......... .......... 47% 8.39M 9s
125200K .......... .......... .......... .......... .......... 47% 7.04M 9s
125250K .......... .......... .......... .......... .......... 47% 7.68M 9s
125300K .......... .......... .......... .......... .......... 47% 7.89M 9s
125350K .......... .......... .......... .......... .......... 47% 7.48M 9s
125400K .......... .......... .......... .......... .......... 47% 7.80M 9s
125450K .......... .......... .......... .......... .......... 47% 7.56M 9s
125500K .......... .......... .......... .......... .......... 47% 7.20M 9s
125550K .......... .......... .......... .......... .......... 47% 7.55M 9s
125600K .......... .......... .......... .......... .......... 47% 7.01M 9s
125650K .......... .......... .......... .......... .......... 47% 8.37M 9s
125700K .......... .......... .......... .......... .......... 47% 7.43M 9s
125750K .......... .......... .......... .......... .......... 47% 9.23M 9s
125800K .......... .......... .......... .......... .......... 47% 6.75M 9s
125850K .......... .......... .......... .......... .......... 47% 8.06M 9s
125900K .......... .......... .......... .......... .......... 47% 11.4M 9s
125950K .......... .......... .......... .......... .......... 47% 6.13M 9s
126000K .......... .......... .......... .......... .......... 47% 12.2M 9s
126050K .......... .......... .......... .......... .......... 47% 5.69M 9s
126100K .......... .......... .......... .......... .......... 47% 11.1M 9s
126150K .......... .......... .......... .......... .......... 47% 6.41M 9s
126200K .......... .......... .......... .......... .......... 47% 9.27M 9s
126250K .......... .......... .......... .......... .......... 47% 11.9M 9s
126300K .......... .......... .......... .......... .......... 47% 5.48M 9s
126350K .......... .......... .......... .......... .......... 47% 11.0M 9s
126400K .......... .......... .......... .......... .......... 47% 6.30M 9s
126450K .......... .......... .......... .......... .......... 47% 9.98M 9s
126500K .......... .......... .......... .......... .......... 47% 6.63M 9s
126550K .......... .......... .......... .......... .......... 47% 8.82M 9s
126600K .......... .......... .......... .......... .......... 47% 7.77M 9s
126650K .......... .......... .......... .......... .......... 47% 10.3M 9s
126700K .......... .......... .......... .......... .......... 47% 7.89M 9s
126750K .......... .......... .......... .......... .......... 47% 9.87M 9s
126800K .......... .......... .......... .......... .......... 47% 9.34M 9s
126850K .......... .......... .......... .......... .......... 47% 6.35M 9s
126900K .......... .......... .......... .......... .......... 47% 10.9M 9s
126950K .......... .......... .......... .......... .......... 47% 6.91M 9s
127000K .......... .......... .......... .......... .......... 47% 7.61M 9s
127050K .......... .......... .......... .......... .......... 47% 10.3M 9s
127100K .......... .......... .......... .......... .......... 47% 6.75M 9s
127150K .......... .......... .......... .......... .......... 47% 8.42M 9s
127200K .......... .......... .......... .......... .......... 47% 6.91M 9s
127250K .......... .......... .......... .......... .......... 47% 13.2M 9s
127300K .......... .......... .......... .......... .......... 47% 8.33M 9s
127350K .......... .......... .......... .......... .......... 47% 6.50M 9s
127400K .......... .......... .......... .......... .......... 47% 12.8M 9s
127450K .......... .......... .......... .......... .......... 47% 5.97M 9s
127500K .......... .......... .......... .......... .......... 47% 11.5M 9s
127550K .......... .......... .......... .......... .......... 48% 6.64M 9s
127600K .......... .......... .......... .......... .......... 48% 10.8M 9s
127650K .......... .......... .......... .......... .......... 48% 7.27M 9s
127700K .......... .......... .......... .......... .......... 48% 7.77M 9s
127750K .......... .......... .......... .......... .......... 48% 8.05M 9s
127800K .......... .......... .......... .......... .......... 48% 7.69M 9s
127850K .......... .......... .......... .......... .......... 48% 11.0M 9s
127900K .......... .......... .......... .......... .......... 48% 6.08M 9s
127950K .......... .......... .......... .......... .......... 48% 9.62M 9s
128000K .......... .......... .......... .......... .......... 48% 8.57M 9s
128050K .......... .......... .......... .......... .......... 48% 6.76M 9s
128100K .......... .......... .......... .......... .......... 48% 7.58M 9s
128150K .......... .......... .......... .......... .......... 48% 9.11M 9s
128200K .......... .......... .......... .......... .......... 48% 10.1M 9s
128250K .......... .......... .......... .......... .......... 48% 6.07M 9s
128300K .......... .......... .......... .......... .......... 48% 10.5M 9s
128350K .......... .......... .......... .......... .......... 48% 7.55M 9s
128400K .......... .......... .......... .......... .......... 48% 7.54M 9s
128450K .......... .......... .......... .......... .......... 48% 12.7M 9s
128500K .......... .......... .......... .......... .......... 48% 5.99M 9s
128550K .......... .......... .......... .......... .......... 48% 10.6M 9s
128600K .......... .......... .......... .......... .......... 48% 7.59M 9s
128650K .......... .......... .......... .......... .......... 48% 7.39M 9s
128700K .......... .......... .......... .......... .......... 48% 7.51M 9s
128750K .......... .......... .......... .......... .......... 48% 6.77M 9s
128800K .......... .......... .......... .......... .......... 48% 17.1M 9s
128850K .......... .......... .......... .......... .......... 48% 5.57M 9s
128900K .......... .......... .......... .......... .......... 48% 10.2M 9s
128950K .......... .......... .......... .......... .......... 48% 7.46M 9s
129000K .......... .......... .......... .......... .......... 48% 6.59M 9s
129050K .......... .......... .......... .......... .......... 48% 23.1M 9s
129100K .......... .......... .......... .......... .......... 48% 5.96M 9s
129150K .......... .......... .......... .......... .......... 48% 8.55M 9s
129200K .......... .......... .......... .......... .......... 48% 6.17M 9s
129250K .......... .......... .......... .......... .......... 48% 7.24M 9s
129300K .......... .......... .......... .......... .......... 48% 22.2M 9s
129350K .......... .......... .......... .......... .......... 48% 5.20M 9s
129400K .......... .......... .......... .......... .......... 48% 11.3M 9s
129450K .......... .......... .......... .......... .......... 48% 7.20M 9s
129500K .......... .......... .......... .......... .......... 48% 6.83M 9s
129550K .......... .......... .......... .......... .......... 48% 15.4M 9s
129600K .......... .......... .......... .......... .......... 48% 5.54M 9s
129650K .......... .......... .......... .......... .......... 48% 11.0M 9s
129700K .......... .......... .......... .......... .......... 48% 13.4M 9s
129750K .......... .......... .......... .......... .......... 48% 5.32M 9s
129800K .......... .......... .......... .......... .......... 48% 12.3M 9s
129850K .......... .......... .......... .......... .......... 48% 5.47M 9s
129900K .......... .......... .......... .......... .......... 48% 10.5M 9s
129950K .......... .......... .......... .......... .......... 48% 13.6M 9s
130000K .......... .......... .......... .......... .......... 48% 5.43M 9s
130050K .......... .......... .......... .......... .......... 48% 12.4M 9s
130100K .......... .......... .......... .......... .......... 48% 9.20M 9s
130150K .......... .......... .......... .......... .......... 48% 5.73M 9s
130200K .......... .......... .......... .......... .......... 49% 15.0M 9s
130250K .......... .......... .......... .......... .......... 49% 5.10M 9s
130300K .......... .......... .......... .......... .......... 49% 15.4M 9s
130350K .......... .......... .......... .......... .......... 49% 8.07M 9s
130400K .......... .......... .......... .......... .......... 49% 5.99M 9s
130450K .......... .......... .......... .......... .......... 49% 15.4M 9s
130500K .......... .......... .......... .......... .......... 49% 4.41M 9s
130550K .......... .......... .......... .......... .......... 49% 12.8M 9s
130600K .......... .......... .......... .......... .......... 49% 17.6M 9s
130650K .......... .......... .......... .......... .......... 49% 4.33M 9s
130700K .......... .......... .......... .......... .......... 49% 15.8M 9s
130750K .......... .......... .......... .......... .......... 49% 11.7M 9s
130800K .......... .......... .......... .......... .......... 49% 5.56M 9s
130850K .......... .......... .......... .......... .......... 49% 11.5M 9s
130900K .......... .......... .......... .......... .......... 49% 6.71M 9s
130950K .......... .......... .......... .......... .......... 49% 7.78M 9s
131000K .......... .......... .......... .......... .......... 49% 16.1M 9s
131050K .......... .......... .......... .......... .......... 49% 4.31M 9s
131100K .......... .......... .......... .......... .......... 49% 14.5M 9s
131150K .......... .......... .......... .......... .......... 49% 23.1M 9s
131200K .......... .......... .......... .......... .......... 49% 4.19M 9s
131250K .......... .......... .......... .......... .......... 49% 15.1M 9s
131300K .......... .......... .......... .......... .......... 49% 8.87M 9s
131350K .......... .......... .......... .......... .......... 49% 5.83M 9s
131400K .......... .......... .......... .......... .......... 49% 12.8M 9s
131450K .......... .......... .......... .......... .......... 49% 5.75M 9s
131500K .......... .......... .......... .......... .......... 49% 8.61M 9s
131550K .......... .......... .......... .......... .......... 49% 16.0M 9s
131600K .......... .......... .......... .......... .......... 49% 5.65M 9s
131650K .......... .......... .......... .......... .......... 49% 10.3M 9s
131700K .......... .......... .......... .......... .......... 49% 8.39M 9s
131750K .......... .......... .......... .......... .......... 49% 7.24M 9s
131800K .......... .......... .......... .......... .......... 49% 9.02M 9s
131850K .......... .......... .......... .......... .......... 49% 10.9M 9s
131900K .......... .......... .......... .......... .......... 49% 7.19M 9s
131950K .......... .......... .......... .......... .......... 49% 9.33M 9s
132000K .......... .......... .......... .......... .......... 49% 10.7M 9s
132050K .......... .......... .......... .......... .......... 49% 6.48M 9s
132100K .......... .......... .......... .......... .......... 49% 11.7M 9s
132150K .......... .......... .......... .......... .......... 49% 8.13M 9s
132200K .......... .......... .......... .......... .......... 49% 6.47M 9s
132250K .......... .......... .......... .......... .......... 49% 12.0M 9s
132300K .......... .......... .......... .......... .......... 49% 7.07M 9s
132350K .......... .......... .......... .......... .......... 49% 7.08M 9s
132400K .......... .......... .......... .......... .......... 49% 11.6M 9s
132450K .......... .......... .......... .......... .......... 49% 7.07M 9s
132500K .......... .......... .......... .......... .......... 49% 8.45M 9s
132550K .......... .......... .......... .......... .......... 49% 9.65M 9s
132600K .......... .......... .......... .......... .......... 49% 8.32M 9s
132650K .......... .......... .......... .......... .......... 49% 7.53M 9s
132700K .......... .......... .......... .......... .......... 49% 9.37M 9s
132750K .......... .......... .......... .......... .......... 49% 7.72M 9s
132800K .......... .......... .......... .......... .......... 49% 9.15M 9s
132850K .......... .......... .......... .......... .......... 50% 7.32M 9s
132900K .......... .......... .......... .......... .......... 50% 12.3M 9s
132950K .......... .......... .......... .......... .......... 50% 7.27M 9s
133000K .......... .......... .......... .......... .......... 50% 8.49M 9s
133050K .......... .......... .......... .......... .......... 50% 8.66M 9s
133100K .......... .......... .......... .......... .......... 50% 8.86M 9s
133150K .......... .......... .......... .......... .......... 50% 8.22M 9s
133200K .......... .......... .......... .......... .......... 50% 8.51M 9s
133250K .......... .......... .......... .......... .......... 50% 7.67M 9s
133300K .......... .......... .......... .......... .......... 50% 11.6M 9s
133350K .......... .......... .......... .......... .......... 50% 7.78M 9s
133400K .......... .......... .......... .......... .......... 50% 7.88M 9s
133450K .......... .......... .......... .......... .......... 50% 9.02M 9s
133500K .......... .......... .......... .......... .......... 50% 8.71M 9s
133550K .......... .......... .......... .......... .......... 50% 7.68M 9s
133600K .......... .......... .......... .......... .......... 50% 10.1M 9s
133650K .......... .......... .......... .......... .......... 50% 6.84M 9s
133700K .......... .......... .......... .......... .......... 50% 7.84M 9s
133750K .......... .......... .......... .......... .......... 50% 12.3M 9s
133800K .......... .......... .......... .......... .......... 50% 6.69M 9s
133850K .......... .......... .......... .......... .......... 50% 7.79M 9s
133900K .......... .......... .......... .......... .......... 50% 12.5M 9s
133950K .......... .......... .......... .......... .......... 50% 5.96M 9s
134000K .......... .......... .......... .......... .......... 50% 10.0M 9s
134050K .......... .......... .......... .......... .......... 50% 13.0M 9s
134100K .......... .......... .......... .......... .......... 50% 7.30M 9s
134150K .......... .......... .......... .......... .......... 50% 7.19M 9s
134200K .......... .......... .......... .......... .......... 50% 14.0M 9s
134250K .......... .......... .......... .......... .......... 50% 7.29M 9s
134300K .......... .......... .......... .......... .......... 50% 8.14M 9s
134350K .......... .......... .......... .......... .......... 50% 10.5M 9s
134400K .......... .......... .......... .......... .......... 50% 6.84M 9s
134450K .......... .......... .......... .......... .......... 50% 6.27M 9s
134500K .......... .......... .......... .......... .......... 50% 20.3M 9s
134550K .......... .......... .......... .......... .......... 50% 8.99M 9s
134600K .......... .......... .......... .......... .......... 50% 4.99M 9s
134650K .......... .......... .......... .......... .......... 50% 24.9M 9s
134700K .......... .......... .......... .......... .......... 50% 7.90M 9s
134750K .......... .......... .......... .......... .......... 50% 6.86M 9s
134800K .......... .......... .......... .......... .......... 50% 12.0M 9s
134850K .......... .......... .......... .......... .......... 50% 9.08M 9s
134900K .......... .......... .......... .......... .......... 50% 5.92M 9s
134950K .......... .......... .......... .......... .......... 50% 13.6M 9s
135000K .......... .......... .......... .......... .......... 50% 8.68M 9s
135050K .......... .......... .......... .......... .......... 50% 2.19M 9s
135100K .......... .......... .......... .......... .......... 50% 26.3M 9s
135150K .......... .......... .......... .......... .......... 50% 57.8M 9s
135200K .......... .......... .......... .......... .......... 50% 18.0M 9s
135250K .......... .......... .......... .......... .......... 50% 18.6M 9s
135300K .......... .......... .......... .......... .......... 50% 6.63M 9s
135350K .......... .......... .......... .......... .......... 50% 8.04M 9s
135400K .......... .......... .......... .......... .......... 50% 9.44M 9s
135450K .......... .......... .......... .......... .......... 50% 6.56M 9s
135500K .......... .......... .......... .......... .......... 51% 10.4M 9s
135550K .......... .......... .......... .......... .......... 51% 6.87M 9s
135600K .......... .......... .......... .......... .......... 51% 12.2M 9s
135650K .......... .......... .......... .......... .......... 51% 7.63M 9s
135700K .......... .......... .......... .......... .......... 51% 11.2M 9s
135750K .......... .......... .......... .......... .......... 51% 7.48M 9s
135800K .......... .......... .......... .......... .......... 51% 14.3M 9s
135850K .......... .......... .......... .......... .......... 51% 6.61M 9s
135900K .......... .......... .......... .......... .......... 51% 15.2M 9s
135950K .......... .......... .......... .......... .......... 51% 11.3M 9s
136000K .......... .......... .......... .......... .......... 51% 7.64M 9s
136050K .......... .......... .......... .......... .......... 51% 15.2M 9s
136100K .......... .......... .......... .......... .......... 51% 7.26M 9s
136150K .......... .......... .......... .......... .......... 51% 12.5M 9s
136200K .......... .......... .......... .......... .......... 51% 6.45M 9s
136250K .......... .......... .......... .......... .......... 51% 13.4M 9s
136300K .......... .......... .......... .......... .......... 51% 9.01M 9s
136350K .......... .......... .......... .......... .......... 51% 12.8M 9s
136400K .......... .......... .......... .......... .......... 51% 5.51M 9s
136450K .......... .......... .......... .......... .......... 51% 4.07M 9s
136500K .......... .......... .......... .......... .......... 51% 11.1M 9s
136550K .......... .......... .......... .......... .......... 51% 12.2M 9s
136600K .......... .......... .......... .......... .......... 51% 7.56M 9s
136650K .......... .......... .......... .......... .......... 51% 14.8M 9s
136700K .......... .......... .......... .......... .......... 51% 13.4M 9s
136750K .......... .......... .......... .......... .......... 51% 19.5M 9s
136800K .......... .......... .......... .......... .......... 51% 26.9M 9s
136850K .......... .......... .......... .......... .......... 51% 13.5M 9s
136900K .......... .......... .......... .......... .......... 51% 3.54M 9s
136950K .......... .......... .......... .......... .......... 51% 5.21M 9s
137000K .......... .......... .......... .......... .......... 51% 1.66M 9s
137050K .......... .......... .......... .......... .......... 51% 8.73M 9s
137100K .......... .......... .......... .......... .......... 51% 47.4M 9s
137150K .......... .......... .......... .......... .......... 51% 49.2M 9s
137200K .......... .......... .......... .......... .......... 51% 41.0M 9s
137250K .......... .......... .......... .......... .......... 51% 47.0M 9s
137300K .......... .......... .......... .......... .......... 51% 24.0M 9s
137350K .......... .......... .......... .......... .......... 51% 32.1M 9s
137400K .......... .......... .......... .......... .......... 51% 12.5M 9s
137450K .......... .......... .......... .......... .......... 51% 10.4M 9s
137500K .......... .......... .......... .......... .......... 51% 11.2M 9s
137550K .......... .......... .......... .......... .......... 51% 15.5M 9s
137600K .......... .......... .......... .......... .......... 51% 8.41M 9s
137650K .......... .......... .......... .......... .......... 51% 24.7M 9s
137700K .......... .......... .......... .......... .......... 51% 8.14M 9s
137750K .......... .......... .......... .......... .......... 51% 15.3M 9s
137800K .......... .......... .......... .......... .......... 51% 9.71M 9s
137850K .......... .......... .......... .......... .......... 51% 13.8M 9s
137900K .......... .......... .......... .......... .......... 51% 9.27M 9s
137950K .......... .......... .......... .......... .......... 51% 10.8M 9s
138000K .......... .......... .......... .......... .......... 51% 12.7M 9s
138050K .......... .......... .......... .......... .......... 51% 8.84M 9s
138100K .......... .......... .......... .......... .......... 51% 13.9M 9s
138150K .......... .......... .......... .......... .......... 52% 10.5M 9s
138200K .......... .......... .......... .......... .......... 52% 10.3M 9s
138250K .......... .......... .......... .......... .......... 52% 9.76M 9s
138300K .......... .......... .......... .......... .......... 52% 14.9M 9s
138350K .......... .......... .......... .......... .......... 52% 7.94M 9s
138400K .......... .......... .......... .......... .......... 52% 10.9M 9s
138450K .......... .......... .......... .......... .......... 52% 11.0M 9s
138500K .......... .......... .......... .......... .......... 52% 11.3M 9s
138550K .......... .......... .......... .......... .......... 52% 14.9M 9s
138600K .......... .......... .......... .......... .......... 52% 6.49M 9s
138650K .......... .......... .......... .......... .......... 52% 12.5M 9s
138700K .......... .......... .......... .......... .......... 52% 6.47M 9s
138750K .......... .......... .......... .......... .......... 52% 9.04M 9s
138800K .......... .......... .......... .......... .......... 52% 8.88M 9s
138850K .......... .......... .......... .......... .......... 52% 6.87M 9s
138900K .......... .......... .......... .......... .......... 52% 9.19M 9s
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139000K .......... .......... .......... .......... .......... 52% 5.44M 9s
139050K .......... .......... .......... .......... .......... 52% 10.3M 9s
139100K .......... .......... .......... .......... .......... 52% 6.24M 9s
139150K .......... .......... .......... .......... .......... 52% 10.6M 9s
139200K .......... .......... .......... .......... .......... 52% 9.95M 9s
139250K .......... .......... .......... .......... .......... 52% 6.10M 9s
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139350K .......... .......... .......... .......... .......... 52% 7.87M 9s
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139450K .......... .......... .......... .......... .......... 52% 9.82M 9s
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139800K .......... .......... .......... .......... .......... 52% 8.46M 9s
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139950K .......... .......... .......... .......... .......... 52% 7.34M 9s
140000K .......... .......... .......... .......... .......... 52% 13.8M 9s
140050K .......... .......... .......... .......... .......... 52% 11.5M 9s
140100K .......... .......... .......... .......... .......... 52% 6.72M 9s
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140200K .......... .......... .......... .......... .......... 52% 8.63M 9s
140250K .......... .......... .......... .......... .......... 52% 9.46M 9s
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140450K .......... .......... .......... .......... .......... 52% 11.1M 9s
140500K .......... .......... .......... .......... .......... 52% 6.99M 9s
140550K .......... .......... .......... .......... .......... 52% 18.3M 9s
140600K .......... .......... .......... .......... .......... 52% 11.0M 9s
140650K .......... .......... .......... .......... .......... 52% 6.55M 9s
140700K .......... .......... .......... .......... .......... 52% 22.1M 9s
140750K .......... .......... .......... .......... .......... 52% 9.13M 9s
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140850K .......... .......... .......... .......... .......... 53% 12.7M 9s
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141000K .......... .......... .......... .......... .......... 53% 9.09M 9s
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141100K .......... .......... .......... .......... .......... 53% 11.7M 9s
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141200K .......... .......... .......... .......... .......... 53% 11.7M 9s
141250K .......... .......... .......... .......... .......... 53% 17.7M 9s
141300K .......... .......... .......... .......... .......... 53% 8.30M 9s
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141400K .......... .......... .......... .......... .......... 53% 19.9M 9s
141450K .......... .......... .......... .......... .......... 53% 8.69M 9s
141500K .......... .......... .......... .......... .......... 53% 7.83M 9s
141550K .......... .......... .......... .......... .......... 53% 33.8M 9s
141600K .......... .......... .......... .......... .......... 53% 8.28M 9s
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141700K .......... .......... .......... .......... .......... 53% 19.7M 9s
141750K .......... .......... .......... .......... .......... 53% 10.4M 9s
141800K .......... .......... .......... .......... .......... 53% 7.99M 9s
141850K .......... .......... .......... .......... .......... 53% 13.7M 9s
141900K .......... .......... .......... .......... .......... 53% 7.85M 9s
141950K .......... .......... .......... .......... .......... 53% 10.7M 9s
142000K .......... .......... .......... .......... .......... 53% 10.0M 9s
142050K .......... .......... .......... .......... .......... 53% 11.4M 9s
142100K .......... .......... .......... .......... .......... 53% 9.66M 9s
142150K .......... .......... .......... .......... .......... 53% 9.19M 9s
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142250K .......... .......... .......... .......... .......... 53% 12.2M 9s
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142400K .......... .......... .......... .......... .......... 53% 12.4M 9s
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142500K .......... .......... .......... .......... .......... 53% 7.27M 9s
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142650K .......... .......... .......... .......... .......... 53% 7.09M 9s
142700K .......... .......... .......... .......... .......... 53% 15.5M 9s
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142800K .......... .......... .......... .......... .......... 53% 7.22M 9s
142850K .......... .......... .......... .......... .......... 53% 12.8M 9s
142900K .......... .......... .......... .......... .......... 53% 14.9M 9s
142950K .......... .......... .......... .......... .......... 53% 7.01M 9s
143000K .......... .......... .......... .......... .......... 53% 14.1M 9s
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143100K .......... .......... .......... .......... .......... 53% 6.65M 9s
143150K .......... .......... .......... .......... .......... 53% 16.8M 9s
143200K .......... .......... .......... .......... .......... 53% 10.3M 8s
143250K .......... .......... .......... .......... .......... 53% 8.19M 8s
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143400K .......... .......... .......... .......... .......... 53% 7.20M 8s
143450K .......... .......... .......... .......... .......... 53% 13.7M 8s
143500K .......... .......... .......... .......... .......... 54% 16.2M 8s
143550K .......... .......... .......... .......... .......... 54% 6.80M 8s
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143700K .......... .......... .......... .......... .......... 54% 6.81M 8s
143750K .......... .......... .......... .......... .......... 54% 16.2M 8s
143800K .......... .......... .......... .......... .......... 54% 14.4M 8s
143850K .......... .......... .......... .......... .......... 54% 6.46M 8s
143900K .......... .......... .......... .......... .......... 54% 17.5M 8s
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144000K .......... .......... .......... .......... .......... 54% 7.22M 8s
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144100K .......... .......... .......... .......... .......... 54% 17.3M 8s
144150K .......... .......... .......... .......... .......... 54% 6.78M 8s
144200K .......... .......... .......... .......... .......... 54% 12.6M 8s
144250K .......... .......... .......... .......... .......... 54% 18.0M 8s
144300K .......... .......... .......... .......... .......... 54% 11.3M 8s
144350K .......... .......... .......... .......... .......... 54% 7.26M 8s
144400K .......... .......... .......... .......... .......... 54% 16.1M 8s
144450K .......... .......... .......... .......... .......... 54% 10.4M 8s
144500K .......... .......... .......... .......... .......... 54% 8.38M 8s
144550K .......... .......... .......... .......... .......... 54% 15.8M 8s
144600K .......... .......... .......... .......... .......... 54% 11.2M 8s
144650K .......... .......... .......... .......... .......... 54% 6.44M 8s
144700K .......... .......... .......... .......... .......... 54% 18.3M 8s
144750K .......... .......... .......... .......... .......... 54% 12.6M 8s
144800K .......... .......... .......... .......... .......... 54% 7.81M 8s
144850K .......... .......... .......... .......... .......... 54% 11.2M 8s
144900K .......... .......... .......... .......... .......... 54% 17.5M 8s
144950K .......... .......... .......... .......... .......... 54% 6.20M 8s
145000K .......... .......... .......... .......... .......... 54% 19.6M 8s
145050K .......... .......... .......... .......... .......... 54% 14.6M 8s
145100K .......... .......... .......... .......... .......... 54% 7.38M 8s
145150K .......... .......... .......... .......... .......... 54% 15.0M 8s
145200K .......... .......... .......... .......... .......... 54% 14.4M 8s
145250K .......... .......... .......... .......... .......... 54% 8.75M 8s
145300K .......... .......... .......... .......... .......... 54% 11.6M 8s
145350K .......... .......... .......... .......... .......... 54% 14.3M 8s
145400K .......... .......... .......... .......... .......... 54% 8.02M 8s
145450K .......... .......... .......... .......... .......... 54% 9.81M 8s
145500K .......... .......... .......... .......... .......... 54% 19.8M 8s
145550K .......... .......... .......... .......... .......... 54% 10.2M 8s
145600K .......... .......... .......... .......... .......... 54% 7.22M 8s
145650K .......... .......... .......... .......... .......... 54% 25.6M 8s
145700K .......... .......... .......... .......... .......... 54% 8.45M 8s
145750K .......... .......... .......... .......... .......... 54% 11.9M 8s
145800K .......... .......... .......... .......... .......... 54% 12.0M 8s
145850K .......... .......... .......... .......... .......... 54% 8.73M 8s
145900K .......... .......... .......... .......... .......... 54% 10.9M 8s
145950K .......... .......... .......... .......... .......... 54% 12.9M 8s
146000K .......... .......... .......... .......... .......... 54% 13.2M 8s
146050K .......... .......... .......... .......... .......... 54% 8.64M 8s
146100K .......... .......... .......... .......... .......... 54% 9.90M 8s
146150K .......... .......... .......... .......... .......... 55% 13.4M 8s
146200K .......... .......... .......... .......... .......... 55% 12.4M 8s
146250K .......... .......... .......... .......... .......... 55% 8.69M 8s
146300K .......... .......... .......... .......... .......... 55% 19.3M 8s
146350K .......... .......... .......... .......... .......... 55% 9.58M 8s
146400K .......... .......... .......... .......... .......... 55% 9.22M 8s
146450K .......... .......... .......... .......... .......... 55% 16.5M 8s
146500K .......... .......... .......... .......... .......... 55% 12.9M 8s
146550K .......... .......... .......... .......... .......... 55% 10.1M 8s
146600K .......... .......... .......... .......... .......... 55% 11.8M 8s
146650K .......... .......... .......... .......... .......... 55% 13.1M 8s
146700K .......... .......... .......... .......... .......... 55% 10.6M 8s
146750K .......... .......... .......... .......... .......... 55% 9.00M 8s
146800K .......... .......... .......... .......... .......... 55% 41.9M 8s
146850K .......... .......... .......... .......... .......... 55% 8.33M 8s
146900K .......... .......... .......... .......... .......... 55% 7.51M 8s
146950K .......... .......... .......... .......... .......... 55% 23.7M 8s
147000K .......... .......... .......... .......... .......... 55% 14.1M 8s
147050K .......... .......... .......... .......... .......... 55% 8.81M 8s
147100K .......... .......... .......... .......... .......... 55% 12.5M 8s
147150K .......... .......... .......... .......... .......... 55% 14.0M 8s
147200K .......... .......... .......... .......... .......... 55% 7.98M 8s
147250K .......... .......... .......... .......... .......... 55% 14.2M 8s
147300K .......... .......... .......... .......... .......... 55% 25.2M 8s
147350K .......... .......... .......... .......... .......... 55% 8.21M 8s
147400K .......... .......... .......... .......... .......... 55% 8.30M 8s
147450K .......... .......... .......... .......... .......... 55% 25.3M 8s
147500K .......... .......... .......... .......... .......... 55% 10.9M 8s
147550K .......... .......... .......... .......... .......... 55% 10.7M 8s
147600K .......... .......... .......... .......... .......... 55% 11.5M 8s
147650K .......... .......... .......... .......... .......... 55% 14.8M 8s
147700K .......... .......... .......... .......... .......... 55% 9.49M 8s
147750K .......... .......... .......... .......... .......... 55% 9.70M 8s
147800K .......... .......... .......... .......... .......... 55% 25.1M 8s
147850K .......... .......... .......... .......... .......... 55% 7.68M 8s
147900K .......... .......... .......... .......... .......... 55% 8.97M 8s
147950K .......... .......... .......... .......... .......... 55% 22.6M 8s
148000K .......... .......... .......... .......... .......... 55% 9.63M 8s
148050K .......... .......... .......... .......... .......... 55% 13.9M 8s
148100K .......... .......... .......... .......... .......... 55% 10.6M 8s
148150K .......... .......... .......... .......... .......... 55% 32.6M 8s
148200K .......... .......... .......... .......... .......... 55% 7.77M 8s
148250K .......... .......... .......... .......... .......... 55% 7.45M 8s
148300K .......... .......... .......... .......... .......... 55% 89.1M 8s
148350K .......... .......... .......... .......... .......... 55% 8.82M 8s
148400K .......... .......... .......... .......... .......... 55% 11.0M 8s
148450K .......... .......... .......... .......... .......... 55% 11.3M 8s
148500K .......... .......... .......... .......... .......... 55% 33.8M 8s
148550K .......... .......... .......... .......... .......... 55% 8.16M 8s
148600K .......... .......... .......... .......... .......... 55% 7.31M 8s
148650K .......... .......... .......... .......... .......... 55% 98.1M 8s
148700K .......... .......... .......... .......... .......... 55% 6.78M 8s
148750K .......... .......... .......... .......... .......... 55% 16.7M 8s
148800K .......... .......... .......... .......... .......... 56% 10.9M 8s
148850K .......... .......... .......... .......... .......... 56% 14.4M 8s
148900K .......... .......... .......... .......... .......... 56% 12.1M 8s
148950K .......... .......... .......... .......... .......... 56% 7.08M 8s
149000K .......... .......... .......... .......... .......... 56% 33.5M 8s
149050K .......... .......... .......... .......... .......... 56% 8.34M 8s
149100K .......... .......... .......... .......... .......... 56% 13.5M 8s
149150K .......... .......... .......... .......... .......... 56% 11.6M 8s
149200K .......... .......... .......... .......... .......... 56% 14.1M 8s
149250K .......... .......... .......... .......... .......... 56% 11.1M 8s
149300K .......... .......... .......... .......... .......... 56% 8.75M 8s
149350K .......... .......... .......... .......... .......... 56% 30.9M 8s
149400K .......... .......... .......... .......... .......... 56% 7.16M 8s
149450K .......... .......... .......... .......... .......... 56% 13.9M 8s
149500K .......... .......... .......... .......... .......... 56% 13.4M 8s
149550K .......... .......... .......... .......... .......... 56% 12.7M 8s
149600K .......... .......... .......... .......... .......... 56% 11.3M 8s
149650K .......... .......... .......... .......... .......... 56% 8.15M 8s
149700K .......... .......... .......... .......... .......... 56% 19.4M 8s
149750K .......... .......... .......... .......... .......... 56% 8.33M 8s
149800K .......... .......... .......... .......... .......... 56% 18.9M 8s
149850K .......... .......... .......... .......... .......... 56% 8.36M 8s
149900K .......... .......... .......... .......... .......... 56% 26.0M 8s
149950K .......... .......... .......... .......... .......... 56% 9.28M 8s
150000K .......... .......... .......... .......... .......... 56% 8.93M 8s
150050K .......... .......... .......... .......... .......... 56% 32.2M 8s
150100K .......... .......... .......... .......... .......... 56% 8.57M 8s
150150K .......... .......... .......... .......... .......... 56% 14.0M 8s
150200K .......... .......... .......... .......... .......... 56% 8.42M 8s
150250K .......... .......... .......... .......... .......... 56% 14.3M 8s
150300K .......... .......... .......... .......... .......... 56% 11.0M 8s
150350K .......... .......... .......... .......... .......... 56% 13.4M 8s
150400K .......... .......... .......... .......... .......... 56% 11.3M 8s
150450K .......... .......... .......... .......... .......... 56% 7.61M 8s
150500K .......... .......... .......... .......... .......... 56% 20.9M 8s
150550K .......... .......... .......... .......... .......... 56% 9.13M 8s
150600K .......... .......... .......... .......... .......... 56% 35.5M 8s
150650K .......... .......... .......... .......... .......... 56% 7.18M 8s
150700K .......... .......... .......... .......... .......... 56% 12.2M 8s
150750K .......... .......... .......... .......... .......... 56% 12.0M 8s
150800K .......... .......... .......... .......... .......... 56% 19.8M 8s
150850K .......... .......... .......... .......... .......... 56% 8.02M 8s
150900K .......... .......... .......... .......... .......... 56% 8.70M 8s
150950K .......... .......... .......... .......... .......... 56% 27.2M 8s
151000K .......... .......... .......... .......... .......... 56% 13.4M 8s
151050K .......... .......... .......... .......... .......... 56% 9.28M 8s
151100K .......... .......... .......... .......... .......... 56% 8.36M 8s
151150K .......... .......... .......... .......... .......... 56% 20.1M 8s
151200K .......... .......... .......... .......... .......... 56% 8.13M 8s
151250K .......... .......... .......... .......... .......... 56% 9.12M 8s
151300K .......... .......... .......... .......... .......... 56% 19.2M 8s
151350K .......... .......... .......... .......... .......... 56% 14.8M 8s
151400K .......... .......... .......... .......... .......... 56% 12.0M 8s
151450K .......... .......... .......... .......... .......... 57% 8.24M 8s
151500K .......... .......... .......... .......... .......... 57% 15.6M 8s
151550K .......... .......... .......... .......... .......... 57% 17.6M 8s
151600K .......... .......... .......... .......... .......... 57% 7.53M 8s
151650K .......... .......... .......... .......... .......... 57% 8.89M 8s
151700K .......... .......... .......... .......... .......... 57% 34.5M 8s
151750K .......... .......... .......... .......... .......... 57% 14.3M 8s
151800K .......... .......... .......... .......... .......... 57% 5.75M 8s
151850K .......... .......... .......... .......... .......... 57% 15.3M 8s
151900K .......... .......... .......... .......... .......... 57% 41.2M 8s
151950K .......... .......... .......... .......... .......... 57% 8.75M 8s
152000K .......... .......... .......... .......... .......... 57% 8.59M 8s
152050K .......... .......... .......... .......... .......... 57% 21.4M 8s
152100K .......... .......... .......... .......... .......... 57% 12.8M 8s
152150K .......... .......... .......... .......... .......... 57% 12.1M 8s
152200K .......... .......... .......... .......... .......... 57% 8.19M 8s
152250K .......... .......... .......... .......... .......... 57% 23.2M 8s
152300K .......... .......... .......... .......... .......... 57% 10.1M 8s
152350K .......... .......... .......... .......... .......... 57% 12.0M 8s
152400K .......... .......... .......... .......... .......... 57% 7.82M 8s
152450K .......... .......... .......... .......... .......... 57% 39.5M 8s
152500K .......... .......... .......... .......... .......... 57% 7.65M 8s
152550K .......... .......... .......... .......... .......... 57% 25.7M 8s
152600K .......... .......... .......... .......... .......... 57% 7.41M 8s
152650K .......... .......... .......... .......... .......... 57% 64.5M 8s
152700K .......... .......... .......... .......... .......... 57% 7.06M 8s
152750K .......... .......... .......... .......... .......... 57% 8.79M 8s
152800K .......... .......... .......... .......... .......... 57% 25.0M 8s
152850K .......... .......... .......... .......... .......... 57% 38.6M 8s
152900K .......... .......... .......... .......... .......... 57% 6.90M 8s
152950K .......... .......... .......... .......... .......... 57% 8.83M 8s
153000K .......... .......... .......... .......... .......... 57% 17.6M 8s
153050K .......... .......... .......... .......... .......... 57% 26.5M 8s
153100K .......... .......... .......... .......... .......... 57% 9.00M 8s
153150K .......... .......... .......... .......... .......... 57% 7.63M 8s
153200K .......... .......... .......... .......... .......... 57% 14.0M 8s
153250K .......... .......... .......... .......... .......... 57% 19.0M 8s
153300K .......... .......... .......... .......... .......... 57% 10.3M 8s
153350K .......... .......... .......... .......... .......... 57% 7.99M 8s
153400K .......... .......... .......... .......... .......... 57% 18.3M 8s
153450K .......... .......... .......... .......... .......... 57% 10.7M 8s
153500K .......... .......... .......... .......... .......... 57% 17.4M 8s
153550K .......... .......... .......... .......... .......... 57% 8.43M 8s
153600K .......... .......... .......... .......... .......... 57% 12.3M 8s
153650K .......... .......... .......... .......... .......... 57% 14.7M 8s
153700K .......... .......... .......... .......... .......... 57% 6.70M 8s
153750K .......... .......... .......... .......... .......... 57% 14.4M 8s
153800K .......... .......... .......... .......... .......... 57% 19.4M 8s
153850K .......... .......... .......... .......... .......... 57% 13.1M 8s
153900K .......... .......... .......... .......... .......... 57% 7.56M 8s
153950K .......... .......... .......... .......... .......... 57% 13.2M 8s
154000K .......... .......... .......... .......... .......... 57% 16.9M 8s
154050K .......... .......... .......... .......... .......... 57% 12.6M 8s
154100K .......... .......... .......... .......... .......... 58% 8.04M 8s
154150K .......... .......... .......... .......... .......... 58% 12.7M 8s
154200K .......... .......... .......... .......... .......... 58% 13.6M 8s
154250K .......... .......... .......... .......... .......... 58% 14.4M 8s
154300K .......... .......... .......... .......... .......... 58% 21.0M 8s
154350K .......... .......... .......... .......... .......... 58% 5.75M 8s
154400K .......... .......... .......... .......... .......... 58% 21.8M 8s
154450K .......... .......... .......... .......... .......... 58% 11.8M 8s
154500K .......... .......... .......... .......... .......... 58% 9.81M 8s
154550K .......... .......... .......... .......... .......... 58% 11.7M 8s
154600K .......... .......... .......... .......... .......... 58% 12.9M 8s
154650K .......... .......... .......... .......... .......... 58% 14.1M 8s
154700K .......... .......... .......... .......... .......... 58% 7.11M 8s
154750K .......... .......... .......... .......... .......... 58% 13.8M 8s
154800K .......... .......... .......... .......... .......... 58% 21.0M 8s
154850K .......... .......... .......... .......... .......... 58% 12.7M 8s
154900K .......... .......... .......... .......... .......... 58% 6.34M 8s
154950K .......... .......... .......... .......... .......... 58% 14.3M 8s
155000K .......... .......... .......... .......... .......... 58% 21.7M 8s
155050K .......... .......... .......... .......... .......... 58% 14.5M 8s
155100K .......... .......... .......... .......... .......... 58% 6.18M 8s
155150K .......... .......... .......... .......... .......... 58% 21.8M 8s
155200K .......... .......... .......... .......... .......... 58% 17.2M 8s
155250K .......... .......... .......... .......... .......... 58% 12.5M 8s
155300K .......... .......... .......... .......... .......... 58% 6.70M 8s
155350K .......... .......... .......... .......... .......... 58% 23.0M 8s
155400K .......... .......... .......... .......... .......... 58% 15.8M 8s
155450K .......... .......... .......... .......... .......... 58% 11.9M 8s
155500K .......... .......... .......... .......... .......... 58% 6.34M 8s
155550K .......... .......... .......... .......... .......... 58% 23.6M 8s
155600K .......... .......... .......... .......... .......... 58% 15.9M 8s
155650K .......... .......... .......... .......... .......... 58% 15.0M 8s
155700K .......... .......... .......... .......... .......... 58% 5.66M 8s
155750K .......... .......... .......... .......... .......... 58% 34.1M 8s
155800K .......... .......... .......... .......... .......... 58% 16.4M 8s
155850K .......... .......... .......... .......... .......... 58% 13.4M 8s
155900K .......... .......... .......... .......... .......... 58% 6.28M 8s
155950K .......... .......... .......... .......... .......... 58% 15.5M 8s
156000K .......... .......... .......... .......... .......... 58% 14.2M 8s
156050K .......... .......... .......... .......... .......... 58% 13.7M 8s
156100K .......... .......... .......... .......... .......... 58% 7.51M 8s
156150K .......... .......... .......... .......... .......... 58% 19.1M 8s
156200K .......... .......... .......... .......... .......... 58% 15.6M 8s
156250K .......... .......... .......... .......... .......... 58% 12.9M 8s
156300K .......... .......... .......... .......... .......... 58% 9.30M 8s
156350K .......... .......... .......... .......... .......... 58% 9.90M 8s
156400K .......... .......... .......... .......... .......... 58% 13.9M 8s
156450K .......... .......... .......... .......... .......... 58% 11.5M 8s
156500K .......... .......... .......... .......... .......... 58% 11.1M 8s
156550K .......... .......... .......... .......... .......... 58% 10.2M 8s
156600K .......... .......... .......... .......... .......... 58% 13.0M 8s
156650K .......... .......... .......... .......... .......... 58% 16.5M 8s
156700K .......... .......... .......... .......... .......... 58% 8.78M 8s
156750K .......... .......... .......... .......... .......... 59% 7.37M 8s
156800K .......... .......... .......... .......... .......... 59% 15.7M 8s
156850K .......... .......... .......... .......... .......... 59% 13.0M 8s
156900K .......... .......... .......... .......... .......... 59% 12.5M 8s
156950K .......... .......... .......... .......... .......... 59% 9.57M 8s
157000K .......... .......... .......... .......... .......... 59% 20.0M 8s
157050K .......... .......... .......... .......... .......... 59% 12.6M 8s
157100K .......... .......... .......... .......... .......... 59% 8.34M 8s
157150K .......... .......... .......... .......... .......... 59% 13.3M 8s
157200K .......... .......... .......... .......... .......... 59% 12.2M 8s
157250K .......... .......... .......... .......... .......... 59% 18.5M 8s
157300K .......... .......... .......... .......... .......... 59% 17.6M 8s
157350K .......... .......... .......... .......... .......... 59% 5.99M 8s
157400K .......... .......... .......... .......... .......... 59% 14.5M 8s
157450K .......... .......... .......... .......... .......... 59% 17.7M 8s
157500K .......... .......... .......... .......... .......... 59% 16.9M 8s
157550K .......... .......... .......... .......... .......... 59% 6.39M 8s
157600K .......... .......... .......... .......... .......... 59% 14.2M 8s
157650K .......... .......... .......... .......... .......... 59% 20.9M 8s
157700K .......... .......... .......... .......... .......... 59% 11.6M 8s
157750K .......... .......... .......... .......... .......... 59% 6.32M 8s
157800K .......... .......... .......... .......... .......... 59% 15.7M 8s
157850K .......... .......... .......... .......... .......... 59% 22.6M 8s
157900K .......... .......... .......... .......... .......... 59% 14.9M 8s
157950K .......... .......... .......... .......... .......... 59% 7.30M 8s
158000K .......... .......... .......... .......... .......... 59% 9.00M 8s
158050K .......... .......... .......... .......... .......... 59% 26.8M 8s
158100K .......... .......... .......... .......... .......... 59% 14.1M 8s
158150K .......... .......... .......... .......... .......... 59% 7.65M 8s
158200K .......... .......... .......... .......... .......... 59% 10.2M 8s
158250K .......... .......... .......... .......... .......... 59% 14.0M 8s
158300K .......... .......... .......... .......... .......... 59% 23.8M 8s
158350K .......... .......... .......... .......... .......... 59% 6.46M 8s
158400K .......... .......... .......... .......... .......... 59% 10.2M 8s
158450K .......... .......... .......... .......... .......... 59% 13.1M 8s
158500K .......... .......... .......... .......... .......... 59% 34.7M 8s
158550K .......... .......... .......... .......... .......... 59% 7.17M 8s
158600K .......... .......... .......... .......... .......... 59% 11.1M 8s
158650K .......... .......... .......... .......... .......... 59% 11.9M 8s
158700K .......... .......... .......... .......... .......... 59% 29.8M 8s
158750K .......... .......... .......... .......... .......... 59% 20.3M 8s
158800K .......... .......... .......... .......... .......... 59% 6.99M 8s
158850K .......... .......... .......... .......... .......... 59% 13.8M 8s
158900K .......... .......... .......... .......... .......... 59% 13.6M 8s
158950K .......... .......... .......... .......... .......... 59% 21.5M 8s
159000K .......... .......... .......... .......... .......... 59% 9.26M 8s
159050K .......... .......... .......... .......... .......... 59% 13.1M 8s
159100K .......... .......... .......... .......... .......... 59% 12.4M 8s
159150K .......... .......... .......... .......... .......... 59% 16.3M 8s
159200K .......... .......... .......... .......... .......... 59% 10.1M 8s
159250K .......... .......... .......... .......... .......... 59% 13.4M 8s
159300K .......... .......... .......... .......... .......... 59% 14.3M 8s
159350K .......... .......... .......... .......... .......... 59% 18.6M 8s
159400K .......... .......... .......... .......... .......... 60% 9.66M 8s
159450K .......... .......... .......... .......... .......... 60% 10.0M 8s
159500K .......... .......... .......... .......... .......... 60% 14.5M 8s
159550K .......... .......... .......... .......... .......... 60% 22.9M 8s
159600K .......... .......... .......... .......... .......... 60% 24.7M 8s
159650K .......... .......... .......... .......... .......... 60% 7.04M 8s
159700K .......... .......... .......... .......... .......... 60% 12.2M 8s
159750K .......... .......... .......... .......... .......... 60% 17.7M 8s
159800K .......... .......... .......... .......... .......... 60% 28.4M 8s
159850K .......... .......... .......... .......... .......... 60% 7.25M 8s
159900K .......... .......... .......... .......... .......... 60% 18.1M 8s
159950K .......... .......... .......... .......... .......... 60% 16.2M 8s
160000K .......... .......... .......... .......... .......... 60% 26.8M 8s
160050K .......... .......... .......... .......... .......... 60% 9.60M 7s
160100K .......... .......... .......... .......... .......... 60% 9.78M 7s
160150K .......... .......... .......... .......... .......... 60% 13.0M 7s
160200K .......... .......... .......... .......... .......... 60% 21.8M 7s
160250K .......... .......... .......... .......... .......... 60% 34.7M 7s
160300K .......... .......... .......... .......... .......... 60% 6.01M 7s
160350K .......... .......... .......... .......... .......... 60% 16.6M 7s
160400K .......... .......... .......... .......... .......... 60% 26.8M 7s
160450K .......... .......... .......... .......... .......... 60% 17.9M 7s
160500K .......... .......... .......... .......... .......... 60% 7.22M 7s
160550K .......... .......... .......... .......... .......... 60% 15.3M 7s
160600K .......... .......... .......... .......... .......... 60% 9.86M 7s
160650K .......... .......... .......... .......... .......... 60% 21.5M 7s
160700K .......... .......... .......... .......... .......... 60% 4.61M 7s
160750K .......... .......... .......... .......... .......... 60% 2.22M 7s
160800K .......... .......... .......... .......... .......... 60% 48.3M 7s
160850K .......... .......... .......... .......... .......... 60% 51.6M 7s
160900K .......... .......... .......... .......... .......... 60% 11.2M 7s
160950K .......... .......... .......... .......... .......... 60% 36.2M 7s
161000K .......... .......... .......... .......... .......... 60% 68.9M 7s
161050K .......... .......... .......... .......... .......... 60% 69.7M 7s
161100K .......... .......... .......... .......... .......... 60% 6.56M 7s
161150K .......... .......... .......... .......... .......... 60% 12.5M 7s
161200K .......... .......... .......... .......... .......... 60% 22.5M 7s
161250K .......... .......... .......... .......... .......... 60% 6.33M 7s
161300K .......... .......... .......... .......... .......... 60% 12.9M 7s
161350K .......... .......... .......... .......... .......... 60% 13.8M 7s
161400K .......... .......... .......... .......... .......... 60% 6.80M 7s
161450K .......... .......... .......... .......... .......... 60% 10.9M 7s
161500K .......... .......... .......... .......... .......... 60% 19.5M 7s
161550K .......... .......... .......... .......... .......... 60% 6.94M 7s
161600K .......... .......... .......... .......... .......... 60% 9.45M 7s
161650K .......... .......... .......... .......... .......... 60% 17.3M 7s
161700K .......... .......... .......... .......... .......... 60% 6.78M 7s
161750K .......... .......... .......... .......... .......... 60% 13.7M 7s
161800K .......... .......... .......... .......... .......... 60% 26.1M 7s
161850K .......... .......... .......... .......... .......... 60% 8.23M 7s
161900K .......... .......... .......... .......... .......... 60% 16.3M 7s
161950K .......... .......... .......... .......... .......... 60% 18.3M 7s
162000K .......... .......... .......... .......... .......... 60% 9.29M 7s
162050K .......... .......... .......... .......... .......... 60% 14.6M 7s
162100K .......... .......... .......... .......... .......... 61% 19.1M 7s
162150K .......... .......... .......... .......... .......... 61% 10.3M 7s
162200K .......... .......... .......... .......... .......... 61% 12.3M 7s
162250K .......... .......... .......... .......... .......... 61% 24.6M 7s
162300K .......... .......... .......... .......... .......... 61% 13.2M 7s
162350K .......... .......... .......... .......... .......... 61% 10.5M 7s
162400K .......... .......... .......... .......... .......... 61% 15.8M 7s
162450K .......... .......... .......... .......... .......... 61% 12.5M 7s
162500K .......... .......... .......... .......... .......... 61% 11.3M 7s
162550K .......... .......... .......... .......... .......... 61% 15.7M 7s
162600K .......... .......... .......... .......... .......... 61% 28.9M 7s
162650K .......... .......... .......... .......... .......... 61% 8.69M 7s
162700K .......... .......... .......... .......... .......... 61% 8.10M 7s
162750K .......... .......... .......... .......... .......... 61% 30.1M 7s
162800K .......... .......... .......... .......... .......... 61% 12.8M 7s
162850K .......... .......... .......... .......... .......... 61% 10.4M 7s
162900K .......... .......... .......... .......... .......... 61% 21.0M 7s
162950K .......... .......... .......... .......... .......... 61% 9.61M 7s
163000K .......... .......... .......... .......... .......... 61% 13.3M 7s
163050K .......... .......... .......... .......... .......... 61% 38.1M 7s
163100K .......... .......... .......... .......... .......... 61% 15.3M 7s
163150K .......... .......... .......... .......... .......... 61% 7.06M 7s
163200K .......... .......... .......... .......... .......... 61% 26.9M 7s
163250K .......... .......... .......... .......... .......... 61% 21.6M 7s
163300K .......... .......... .......... .......... .......... 61% 11.4M 7s
163350K .......... .......... .......... .......... .......... 61% 11.0M 7s
163400K .......... .......... .......... .......... .......... 61% 16.1M 7s
163450K .......... .......... .......... .......... .......... 61% 9.02M 7s
163500K .......... .......... .......... .......... .......... 61% 13.6M 7s
163550K .......... .......... .......... .......... .......... 61% 30.8M 7s
163600K .......... .......... .......... .......... .......... 61% 8.14M 7s
163650K .......... .......... .......... .......... .......... 61% 11.8M 7s
163700K .......... .......... .......... .......... .......... 61% 41.7M 7s
163750K .......... .......... .......... .......... .......... 61% 10.4M 7s
163800K .......... .......... .......... .......... .......... 61% 10.0M 7s
163850K .......... .......... .......... .......... .......... 61% 19.5M 7s
163900K .......... .......... .......... .......... .......... 61% 14.3M 7s
163950K .......... .......... .......... .......... .......... 61% 7.76M 7s
164000K .......... .......... .......... .......... .......... 61% 29.7M 7s
164050K .......... .......... .......... .......... .......... 61% 13.4M 7s
164100K .......... .......... .......... .......... .......... 61% 10.3M 7s
164150K .......... .......... .......... .......... .......... 61% 14.1M 7s
164200K .......... .......... .......... .......... .......... 61% 23.1M 7s
164250K .......... .......... .......... .......... .......... 61% 10.7M 7s
164300K .......... .......... .......... .......... .......... 61% 9.62M 7s
164350K .......... .......... .......... .......... .......... 61% 18.3M 7s
164400K .......... .......... .......... .......... .......... 61% 12.6M 7s
164450K .......... .......... .......... .......... .......... 61% 9.54M 7s
164500K .......... .......... .......... .......... .......... 61% 22.8M 7s
164550K .......... .......... .......... .......... .......... 61% 14.2M 7s
164600K .......... .......... .......... .......... .......... 61% 7.77M 7s
164650K .......... .......... .......... .......... .......... 61% 18.7M 7s
164700K .......... .......... .......... .......... .......... 61% 13.7M 7s
164750K .......... .......... .......... .......... .......... 62% 12.0M 7s
164800K .......... .......... .......... .......... .......... 62% 13.4M 7s
164850K .......... .......... .......... .......... .......... 62% 17.6M 7s
164900K .......... .......... .......... .......... .......... 62% 15.2M 7s
164950K .......... .......... .......... .......... .......... 62% 8.81M 7s
165000K .......... .......... .......... .......... .......... 62% 16.4M 7s
165050K .......... .......... .......... .......... .......... 62% 13.7M 7s
165100K .......... .......... .......... .......... .......... 62% 12.1M 7s
165150K .......... .......... .......... .......... .......... 62% 9.60M 7s
165200K .......... .......... .......... .......... .......... 62% 16.0M 7s
165250K .......... .......... .......... .......... .......... 62% 14.1M 7s
165300K .......... .......... .......... .......... .......... 62% 15.6M 7s
165350K .......... .......... .......... .......... .......... 62% 11.6M 7s
165400K .......... .......... .......... .......... .......... 62% 12.4M 7s
165450K .......... .......... .......... .......... .......... 62% 18.2M 7s
165500K .......... .......... .......... .......... .......... 62% 12.9M 7s
165550K .......... .......... .......... .......... .......... 62% 13.5M 7s
165600K .......... .......... .......... .......... .......... 62% 11.3M 7s
165650K .......... .......... .......... .......... .......... 62% 22.3M 7s
165700K .......... .......... .......... .......... .......... 62% 11.2M 7s
165750K .......... .......... .......... .......... .......... 62% 11.0M 7s
165800K .......... .......... .......... .......... .......... 62% 22.0M 7s
165850K .......... .......... .......... .......... .......... 62% 10.2M 7s
165900K .......... .......... .......... .......... .......... 62% 10.7M 7s
165950K .......... .......... .......... .......... .......... 62% 19.5M 7s
166000K .......... .......... .......... .......... .......... 62% 13.4M 7s
166050K .......... .......... .......... .......... .......... 62% 18.9M 7s
166100K .......... .......... .......... .......... .......... 62% 10.6M 7s
166150K .......... .......... .......... .......... .......... 62% 13.8M 7s
166200K .......... .......... .......... .......... .......... 62% 11.3M 7s
166250K .......... .......... .......... .......... .......... 62% 13.3M 7s
166300K .......... .......... .......... .......... .......... 62% 20.0M 7s
166350K .......... .......... .......... .......... .......... 62% 10.8M 7s
166400K .......... .......... .......... .......... .......... 62% 25.8M 7s
166450K .......... .......... .......... .......... .......... 62% 9.94M 7s
166500K .......... .......... .......... .......... .......... 62% 14.8M 7s
166550K .......... .......... .......... .......... .......... 62% 11.2M 7s
166600K .......... .......... .......... .......... .......... 62% 10.8M 7s
166650K .......... .......... .......... .......... .......... 62% 21.0M 7s
166700K .......... .......... .......... .......... .......... 62% 9.31M 7s
166750K .......... .......... .......... .......... .......... 62% 52.7M 7s
166800K .......... .......... .......... .......... .......... 62% 11.5M 7s
166850K .......... .......... .......... .......... .......... 62% 8.32M 7s
166900K .......... .......... .......... .......... .......... 62% 20.0M 7s
166950K .......... .......... .......... .......... .......... 62% 11.7M 7s
167000K .......... .......... .......... .......... .......... 62% 20.9M 7s
167050K .......... .......... .......... .......... .......... 62% 8.75M 7s
167100K .......... .......... .......... .......... .......... 62% 85.3M 7s
167150K .......... .......... .......... .......... .......... 62% 9.47M 7s
167200K .......... .......... .......... .......... .......... 62% 11.0M 7s
167250K .......... .......... .......... .......... .......... 62% 17.4M 7s
167300K .......... .......... .......... .......... .......... 62% 13.2M 7s
167350K .......... .......... .......... .......... .......... 62% 15.1M 7s
167400K .......... .......... .......... .......... .......... 63% 9.63M 7s
167450K .......... .......... .......... .......... .......... 63% 26.5M 7s
167500K .......... .......... .......... .......... .......... 63% 12.4M 7s
167550K .......... .......... .......... .......... .......... 63% 13.2M 7s
167600K .......... .......... .......... .......... .......... 63% 12.9M 7s
167650K .......... .......... .......... .......... .......... 63% 13.0M 7s
167700K .......... .......... .......... .......... .......... 63% 15.2M 7s
167750K .......... .......... .......... .......... .......... 63% 9.23M 7s
167800K .......... .......... .......... .......... .......... 63% 46.7M 7s
167850K .......... .......... .......... .......... .......... 63% 9.14M 7s
167900K .......... .......... .......... .......... .......... 63% 13.7M 7s
167950K .......... .......... .......... .......... .......... 63% 14.0M 7s
168000K .......... .......... .......... .......... .......... 63% 11.9M 7s
168050K .......... .......... .......... .......... .......... 63% 17.3M 7s
168100K .......... .......... .......... .......... .......... 63% 12.5M 7s
168150K .......... .......... .......... .......... .......... 63% 17.6M 7s
168200K .......... .......... .......... .......... .......... 63% 8.58M 7s
168250K .......... .......... .......... .......... .......... 63% 14.4M 7s
168300K .......... .......... .......... .......... .......... 63% 15.2M 7s
168350K .......... .......... .......... .......... .......... 63% 10.8M 7s
168400K .......... .......... .......... .......... .......... 63% 15.8M 7s
168450K .......... .......... .......... .......... .......... 63% 9.48M 7s
168500K .......... .......... .......... .......... .......... 63% 21.6M 7s
168550K .......... .......... .......... .......... .......... 63% 11.3M 7s
168600K .......... .......... .......... .......... .......... 63% 12.0M 7s
168650K .......... .......... .......... .......... .......... 63% 3.00M 7s
168700K .......... .......... .......... .......... .......... 63% 48.7M 7s
168750K .......... .......... .......... .......... .......... 63% 27.0M 7s
168800K .......... .......... .......... .......... .......... 63% 20.9M 7s
168850K .......... .......... .......... .......... .......... 63% 56.5M 7s
168900K .......... .......... .......... .......... .......... 63% 144M 7s
168950K .......... .......... .......... .......... .......... 63% 9.30M 7s
169000K .......... .......... .......... .......... .......... 63% 12.6M 7s
169050K .......... .......... .......... .......... .......... 63% 8.44M 7s
169100K .......... .......... .......... .......... .......... 63% 13.0M 7s
169150K .......... .......... .......... .......... .......... 63% 11.0M 7s
169200K .......... .......... .......... .......... .......... 63% 7.67M 7s
169250K .......... .......... .......... .......... .......... 63% 17.5M 7s
169300K .......... .......... .......... .......... .......... 63% 9.69M 7s
169350K .......... .......... .......... .......... .......... 63% 11.8M 7s
169400K .......... .......... .......... .......... .......... 63% 12.5M 7s
169450K .......... .......... .......... .......... .......... 63% 8.09M 7s
169500K .......... .......... .......... .......... .......... 63% 34.5M 7s
169550K .......... .......... .......... .......... .......... 63% 6.97M 7s
169600K .......... .......... .......... .......... .......... 63% 12.8M 7s
169650K .......... .......... .......... .......... .......... 63% 12.5M 7s
169700K .......... .......... .......... .......... .......... 63% 7.74M 7s
169750K .......... .......... .......... .......... .......... 63% 34.7M 7s
169800K .......... .......... .......... .......... .......... 63% 7.43M 7s
169850K .......... .......... .......... .......... .......... 63% 12.6M 7s
169900K .......... .......... .......... .......... .......... 63% 12.9M 7s
169950K .......... .......... .......... .......... .......... 63% 7.63M 7s
170000K .......... .......... .......... .......... .......... 63% 29.6M 7s
170050K .......... .......... .......... .......... .......... 64% 9.52M 7s
170100K .......... .......... .......... .......... .......... 64% 9.80M 7s
170150K .......... .......... .......... .......... .......... 64% 16.0M 7s
170200K .......... .......... .......... .......... .......... 64% 8.80M 7s
170250K .......... .......... .......... .......... .......... 64% 12.3M 7s
170300K .......... .......... .......... .......... .......... 64% 13.4M 7s
170350K .......... .......... .......... .......... .......... 64% 7.15M 7s
170400K .......... .......... .......... .......... .......... 64% 38.3M 7s
170450K .......... .......... .......... .......... .......... 64% 6.96M 7s
170500K .......... .......... .......... .......... .......... 64% 14.0M 7s
170550K .......... .......... .......... .......... .......... 64% 12.4M 7s
170600K .......... .......... .......... .......... .......... 64% 7.39M 7s
170650K .......... .......... .......... .......... .......... 64% 28.4M 7s
170700K .......... .......... .......... .......... .......... 64% 11.7M 7s
170750K .......... .......... .......... .......... .......... 64% 6.90M 7s
170800K .......... .......... .......... .......... .......... 64% 14.7M 7s
170850K .......... .......... .......... .......... .......... 64% 12.4M 7s
170900K .......... .......... .......... .......... .......... 64% 12.1M 7s
170950K .......... .......... .......... .......... .......... 64% 12.5M 7s
171000K .......... .......... .......... .......... .......... 64% 9.97M 7s
171050K .......... .......... .......... .......... .......... 64% 20.0M 7s
171100K .......... .......... .......... .......... .......... 64% 13.9M 7s
171150K .......... .......... .......... .......... .......... 64% 8.63M 7s
171200K .......... .......... .......... .......... .......... 64% 22.4M 7s
171250K .......... .......... .......... .......... .......... 64% 15.6M 7s
171300K .......... .......... .......... .......... .......... 64% 7.46M 7s
171350K .......... .......... .......... .......... .......... 64% 16.7M 7s
171400K .......... .......... .......... .......... .......... 64% 27.4M 7s
171450K .......... .......... .......... .......... .......... 64% 6.30M 7s
171500K .......... .......... .......... .......... .......... 64% 17.4M 7s
171550K .......... .......... .......... .......... .......... 64% 12.3M 7s
171600K .......... .......... .......... .......... .......... 64% 11.3M 7s
171650K .......... .......... .......... .......... .......... 64% 14.9M 7s
171700K .......... .......... .......... .......... .......... 64% 8.76M 7s
171750K .......... .......... .......... .......... .......... 64% 17.8M 7s
171800K .......... .......... .......... .......... .......... 64% 15.2M 7s
171850K .......... .......... .......... .......... .......... 64% 7.27M 7s
171900K .......... .......... .......... .......... .......... 64% 35.6M 7s
171950K .......... .......... .......... .......... .......... 64% 12.3M 7s
172000K .......... .......... .......... .......... .......... 64% 7.81M 7s
172050K .......... .......... .......... .......... .......... 64% 17.0M 7s
172100K .......... .......... .......... .......... .......... 64% 20.3M 7s
172150K .......... .......... .......... .......... .......... 64% 7.00M 7s
172200K .......... .......... .......... .......... .......... 64% 15.1M 7s
172250K .......... .......... .......... .......... .......... 64% 12.1M 7s
172300K .......... .......... .......... .......... .......... 64% 11.4M 7s
172350K .......... .......... .......... .......... .......... 64% 13.3M 7s
172400K .......... .......... .......... .......... .......... 64% 8.64M 7s
172450K .......... .......... .......... .......... .......... 64% 22.3M 7s
172500K .......... .......... .......... .......... .......... 64% 13.0M 7s
172550K .......... .......... .......... .......... .......... 64% 8.05M 7s
172600K .......... .......... .......... .......... .......... 64% 12.7M 7s
172650K .......... .......... .......... .......... .......... 64% 25.8M 7s
172700K .......... .......... .......... .......... .......... 65% 7.36M 7s
172750K .......... .......... .......... .......... .......... 65% 15.1M 7s
172800K .......... .......... .......... .......... .......... 65% 19.6M 7s
172850K .......... .......... .......... .......... .......... 65% 7.10M 7s
172900K .......... .......... .......... .......... .......... 65% 19.2M 7s
172950K .......... .......... .......... .......... .......... 65% 21.3M 7s
173000K .......... .......... .......... .......... .......... 65% 6.65M 7s
173050K .......... .......... .......... .......... .......... 65% 15.2M 7s
173100K .......... .......... .......... .......... .......... 65% 37.5M 7s
173150K .......... .......... .......... .......... .......... 65% 6.83M 7s
173200K .......... .......... .......... .......... .......... 65% 13.6M 7s
173250K .......... .......... .......... .......... .......... 65% 46.7M 7s
173300K .......... .......... .......... .......... .......... 65% 6.53M 7s
173350K .......... .......... .......... .......... .......... 65% 16.3M 7s
173400K .......... .......... .......... .......... .......... 65% 14.8M 7s
173450K .......... .......... .......... .......... .......... 65% 10.2M 7s
173500K .......... .......... .......... .......... .......... 65% 12.6M 7s
173550K .......... .......... .......... .......... .......... 65% 22.5M 7s
173600K .......... .......... .......... .......... .......... 65% 10.1M 7s
173650K .......... .......... .......... .......... .......... 65% 13.8M 7s
173700K .......... .......... .......... .......... .......... 65% 14.5M 7s
173750K .......... .......... .......... .......... .......... 65% 10.9M 7s
173800K .......... .......... .......... .......... .......... 65% 17.4M 7s
173850K .......... .......... .......... .......... .......... 65% 15.4M 7s
173900K .......... .......... .......... .......... .......... 65% 9.61M 7s
173950K .......... .......... .......... .......... .......... 65% 3.47M 7s
174000K .......... .......... .......... .......... .......... 65% 29.1M 7s
174050K .......... .......... .......... .......... .......... 65% 23.3M 7s
174100K .......... .......... .......... .......... .......... 65% 34.8M 7s
174150K .......... .......... .......... .......... .......... 65% 40.0M 7s
174200K .......... .......... .......... .......... .......... 65% 9.73M 7s
174250K .......... .......... .......... .......... .......... 65% 9.34M 7s
174300K .......... .......... .......... .......... .......... 65% 9.74M 7s
174350K .......... .......... .......... .......... .......... 65% 12.1M 7s
174400K .......... .......... .......... .......... .......... 65% 7.45M 7s
174450K .......... .......... .......... .......... .......... 65% 12.4M 7s
174500K .......... .......... .......... .......... .......... 65% 7.50M 7s
174550K .......... .......... .......... .......... .......... 65% 22.7M 7s
174600K .......... .......... .......... .......... .......... 65% 5.99M 7s
174650K .......... .......... .......... .......... .......... 65% 31.4M 7s
174700K .......... .......... .......... .......... .......... 65% 5.91M 7s
174750K .......... .......... .......... .......... .......... 65% 21.0M 7s
174800K .......... .......... .......... .......... .......... 65% 8.56M 7s
174850K .......... .......... .......... .......... .......... 65% 9.80M 7s
174900K .......... .......... .......... .......... .......... 65% 8.75M 7s
174950K .......... .......... .......... .......... .......... 65% 10.9M 7s
175000K .......... .......... .......... .......... .......... 65% 7.92M 7s
175050K .......... .......... .......... .......... .......... 65% 11.0M 7s
175100K .......... .......... .......... .......... .......... 65% 7.45M 7s
175150K .......... .......... .......... .......... .......... 65% 11.2M 7s
175200K .......... .......... .......... .......... .......... 65% 11.4M 7s
175250K .......... .......... .......... .......... .......... 65% 7.55M 6s
175300K .......... .......... .......... .......... .......... 65% 16.1M 6s
175350K .......... .......... .......... .......... .......... 66% 7.26M 6s
175400K .......... .......... .......... .......... .......... 66% 13.4M 6s
175450K .......... .......... .......... .......... .......... 66% 7.32M 6s
175500K .......... .......... .......... .......... .......... 66% 11.4M 6s
175550K .......... .......... .......... .......... .......... 66% 8.03M 6s
175600K .......... .......... .......... .......... .......... 66% 12.9M 6s
175650K .......... .......... .......... .......... .......... 66% 7.95M 6s
175700K .......... .......... .......... .......... .......... 66% 9.49M 6s
175750K .......... .......... .......... .......... .......... 66% 12.6M 6s
175800K .......... .......... .......... .......... .......... 66% 8.93M 6s
175850K .......... .......... .......... .......... .......... 66% 14.0M 6s
175900K .......... .......... .......... .......... .......... 66% 7.78M 6s
175950K .......... .......... .......... .......... .......... 66% 11.2M 6s
176000K .......... .......... .......... .......... .......... 66% 3.50M 6s
176050K .......... .......... .......... .......... .......... 66% 94.9M 6s
176100K .......... .......... .......... .......... .......... 66% 40.6M 6s
176150K .......... .......... .......... .......... .......... 66% 11.1M 6s
176200K .......... .......... .......... .......... .......... 66% 4.80M 6s
176250K .......... .......... .......... .......... .......... 66% 15.2M 6s
176300K .......... .......... .......... .......... .......... 66% 6.83M 6s
176350K .......... .......... .......... .......... .......... 66% 7.51M 6s
176400K .......... .......... .......... .......... .......... 66% 11.3M 6s
176450K .......... .......... .......... .......... .......... 66% 5.92M 6s
176500K .......... .......... .......... .......... .......... 66% 11.3M 6s
176550K .......... .......... .......... .......... .......... 66% 9.79M 6s
176600K .......... .......... .......... .......... .......... 66% 7.57M 6s
176650K .......... .......... .......... .......... .......... 66% 11.2M 6s
176700K .......... .......... .......... .......... .......... 66% 5.75M 6s
176750K .......... .......... .......... .......... .......... 66% 9.25M 6s
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176850K .......... .......... .......... .......... .......... 66% 6.05M 6s
176900K .......... .......... .......... .......... .......... 66% 14.0M 6s
176950K .......... .......... .......... .......... .......... 66% 6.83M 6s
177000K .......... .......... .......... .......... .......... 66% 8.97M 6s
177050K .......... .......... .......... .......... .......... 66% 9.15M 6s
177100K .......... .......... .......... .......... .......... 66% 5.44M 6s
177150K .......... .......... .......... .......... .......... 66% 23.6M 6s
177200K .......... .......... .......... .......... .......... 66% 5.50M 6s
177250K .......... .......... .......... .......... .......... 66% 9.49M 6s
177300K .......... .......... .......... .......... .......... 66% 8.74M 6s
177350K .......... .......... .......... .......... .......... 66% 4.99M 6s
177400K .......... .......... .......... .......... .......... 66% 28.0M 6s
177450K .......... .......... .......... .......... .......... 66% 4.59M 6s
177500K .......... .......... .......... .......... .......... 66% 35.6M 6s
177550K .......... .......... .......... .......... .......... 66% 5.47M 6s
177600K .......... .......... .......... .......... .......... 66% 9.55M 6s
177650K .......... .......... .......... .......... .......... 66% 12.2M 6s
177700K .......... .......... .......... .......... .......... 66% 5.22M 6s
177750K .......... .......... .......... .......... .......... 66% 15.0M 6s
177800K .......... .......... .......... .......... .......... 66% 7.29M 6s
177850K .......... .......... .......... .......... .......... 66% 11.7M 6s
177900K .......... .......... .......... .......... .......... 66% 6.93M 6s
177950K .......... .......... .......... .......... .......... 66% 13.6M 6s
178000K .......... .......... .......... .......... .......... 67% 8.06M 6s
178050K .......... .......... .......... .......... .......... 67% 17.1M 6s
178100K .......... .......... .......... .......... .......... 67% 5.55M 6s
178150K .......... .......... .......... .......... .......... 67% 16.0M 6s
178200K .......... .......... .......... .......... .......... 67% 6.47M 6s
178250K .......... .......... .......... .......... .......... 67% 14.8M 6s
178300K .......... .......... .......... .......... .......... 67% 6.53M 6s
178350K .......... .......... .......... .......... .......... 67% 14.3M 6s
178400K .......... .......... .......... .......... .......... 67% 6.27M 6s
178450K .......... .......... .......... .......... .......... 67% 12.8M 6s
178500K .......... .......... .......... .......... .......... 67% 6.22M 6s
178550K .......... .......... .......... .......... .......... 67% 11.7M 6s
178600K .......... .......... .......... .......... .......... 67% 6.97M 6s
178650K .......... .......... .......... .......... .......... 67% 11.4M 6s
178700K .......... .......... .......... .......... .......... 67% 6.38M 6s
178750K .......... .......... .......... .......... .......... 67% 7.34M 6s
178800K .......... .......... .......... .......... .......... 67% 13.9M 6s
178850K .......... .......... .......... .......... .......... 67% 5.86M 6s
178900K .......... .......... .......... .......... .......... 67% 17.0M 6s
178950K .......... .......... .......... .......... .......... 67% 6.83M 6s
179000K .......... .......... .......... .......... .......... 67% 11.2M 6s
179050K .......... .......... .......... .......... .......... 67% 15.2M 6s
179100K .......... .......... .......... .......... .......... 67% 6.17M 6s
179150K .......... .......... .......... .......... .......... 67% 10.1M 6s
179200K .......... .......... .......... .......... .......... 67% 7.29M 6s
179250K .......... .......... .......... .......... .......... 67% 9.51M 6s
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179500K .......... .......... .......... .......... .......... 67% 11.6M 6s
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180000K .......... .......... .......... .......... .......... 67% 6.90M 6s
180050K .......... .......... .......... .......... .......... 67% 11.1M 6s
180100K .......... .......... .......... .......... .......... 67% 6.37M 6s
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180200K .......... .......... .......... .......... .......... 67% 6.50M 6s
180250K .......... .......... .......... .......... .......... 67% 10.9M 6s
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181000K .......... .......... .......... .......... .......... 68% 7.13M 6s
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181100K .......... .......... .......... .......... .......... 68% 6.20M 6s
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181200K .......... .......... .......... .......... .......... 68% 6.97M 6s
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181500K .......... .......... .......... .......... .......... 68% 9.50M 6s
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181600K .......... .......... .......... .......... .......... 68% 6.91M 6s
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182000K .......... .......... .......... .......... .......... 68% 12.8M 6s
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182150K .......... .......... .......... .......... .......... 68% 10.2M 6s
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182250K .......... .......... .......... .......... .......... 68% 13.2M 6s
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183000K .......... .......... .......... .......... .......... 68% 14.9M 6s
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183100K .......... .......... .......... .......... .......... 68% 13.0M 6s
183150K .......... .......... .......... .......... .......... 68% 10.4M 6s
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183250K .......... .......... .......... .......... .......... 68% 10.4M 6s
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184000K .......... .......... .......... .......... .......... 69% 15.9M 6s
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184150K .......... .......... .......... .......... .......... 69% 22.1M 6s
184200K .......... .......... .......... .......... .......... 69% 5.05M 6s
184250K .......... .......... .......... .......... .......... 69% 9.60M 6s
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184400K .......... .......... .......... .......... .......... 69% 24.0M 6s
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185000K .......... .......... .......... .......... .......... 69% 6.33M 6s
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185100K .......... .......... .......... .......... .......... 69% 13.3M 6s
185150K .......... .......... .......... .......... .......... 69% 8.15M 6s
185200K .......... .......... .......... .......... .......... 69% 6.61M 6s
185250K .......... .......... .......... .......... .......... 69% 15.2M 6s
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185400K .......... .......... .......... .......... .......... 69% 12.8M 6s
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186000K .......... .......... .......... .......... .......... 70% 5.64M 6s
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186100K .......... .......... .......... .......... .......... 70% 10.3M 6s
186150K .......... .......... .......... .......... .......... 70% 6.66M 6s
186200K .......... .......... .......... .......... .......... 70% 14.2M 6s
186250K .......... .......... .......... .......... .......... 70% 11.0M 6s
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186500K .......... .......... .......... .......... .......... 70% 36.0M 6s
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186650K .......... .......... .......... .......... .......... 70% 44.6M 6s
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186800K .......... .......... .......... .......... .......... 70% 27.9M 6s
186850K .......... .......... .......... .......... .......... 70% 10.0M 6s
186900K .......... .......... .......... .......... .......... 70% 5.70M 6s
186950K .......... .......... .......... .......... .......... 70% 24.3M 6s
187000K .......... .......... .......... .......... .......... 70% 8.92M 6s
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187100K .......... .......... .......... .......... .......... 70% 72.4M 6s
187150K .......... .......... .......... .......... .......... 70% 8.05M 6s
187200K .......... .......... .......... .......... .......... 70% 5.13M 6s
187250K .......... .......... .......... .......... .......... 70% 74.4M 6s
187300K .......... .......... .......... .......... .......... 70% 7.25M 6s
187350K .......... .......... .......... .......... .......... 70% 5.68M 6s
187400K .......... .......... .......... .......... .......... 70% 31.1M 6s
187450K .......... .......... .......... .......... .......... 70% 4.91M 6s
187500K .......... .......... .......... .......... .......... 70% 11.3M 6s
187550K .......... .......... .......... .......... .......... 70% 29.0M 6s
187600K .......... .......... .......... .......... .......... 70% 8.04M 6s
187650K .......... .......... .......... .......... .......... 70% 5.79M 6s
187700K .......... .......... .......... .......... .......... 70% 14.8M 6s
187750K .......... .......... .......... .......... .......... 70% 11.0M 6s
187800K .......... .......... .......... .......... .......... 70% 5.57M 6s
187850K .......... .......... .......... .......... .......... 70% 16.8M 6s
187900K .......... .......... .......... .......... .......... 70% 10.6M 6s
187950K .......... .......... .......... .......... .......... 70% 5.77M 6s
188000K .......... .......... .......... .......... .......... 70% 17.4M 6s
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188100K .......... .......... .......... .......... .......... 70% 4.96M 6s
188150K .......... .......... .......... .......... .......... 70% 23.7M 6s
188200K .......... .......... .......... .......... .......... 70% 8.33M 6s
188250K .......... .......... .......... .......... .......... 70% 5.80M 6s
188300K .......... .......... .......... .......... .......... 70% 27.9M 6s
188350K .......... .......... .......... .......... .......... 70% 8.13M 6s
188400K .......... .......... .......... .......... .......... 70% 5.99M 6s
188450K .......... .......... .......... .......... .......... 70% 21.7M 6s
188500K .......... .......... .......... .......... .......... 70% 10.3M 6s
188550K .......... .......... .......... .......... .......... 70% 5.04M 6s
188600K .......... .......... .......... .......... .......... 70% 27.6M 6s
188650K .......... .......... .......... .......... .......... 71% 10.5M 6s
188700K .......... .......... .......... .......... .......... 71% 4.74M 6s
188750K .......... .......... .......... .......... .......... 71% 31.3M 6s
188800K .......... .......... .......... .......... .......... 71% 12.8M 6s
188850K .......... .......... .......... .......... .......... 71% 4.27M 6s
188900K .......... .......... .......... .......... .......... 71% 48.0M 6s
188950K .......... .......... .......... .......... .......... 71% 11.5M 6s
189000K .......... .......... .......... .......... .......... 71% 4.61M 6s
189050K .......... .......... .......... .......... .......... 71% 35.1M 6s
189100K .......... .......... .......... .......... .......... 71% 11.0M 6s
189150K .......... .......... .......... .......... .......... 71% 6.50M 6s
189200K .......... .......... .......... .......... .......... 71% 9.82M 6s
189250K .......... .......... .......... .......... .......... 71% 12.1M 6s
189300K .......... .......... .......... .......... .......... 71% 12.6M 6s
189350K .......... .......... .......... .......... .......... 71% 5.63M 6s
189400K .......... .......... .......... .......... .......... 71% 15.5M 6s
189450K .......... .......... .......... .......... .......... 71% 11.6M 6s
189500K .......... .......... .......... .......... .......... 71% 5.31M 6s
189550K .......... .......... .......... .......... .......... 71% 38.0M 6s
189600K .......... .......... .......... .......... .......... 71% 7.76M 6s
189650K .......... .......... .......... .......... .......... 71% 5.45M 6s
189700K .......... .......... .......... .......... .......... 71% 26.0M 6s
189750K .......... .......... .......... .......... .......... 71% 10.0M 6s
189800K .......... .......... .......... .......... .......... 71% 5.29M 6s
189850K .......... .......... .......... .......... .......... 71% 20.0M 6s
189900K .......... .......... .......... .......... .......... 71% 13.6M 6s
189950K .......... .......... .......... .......... .......... 71% 5.48M 6s
190000K .......... .......... .......... .......... .......... 71% 10.8M 6s
190050K .......... .......... .......... .......... .......... 71% 12.8M 6s
190100K .......... .......... .......... .......... .......... 71% 6.50M 6s
190150K .......... .......... .......... .......... .......... 71% 8.70M 6s
190200K .......... .......... .......... .......... .......... 71% 16.8M 6s
190250K .......... .......... .......... .......... .......... 71% 6.50M 6s
190300K .......... .......... .......... .......... .......... 71% 11.6M 6s
190350K .......... .......... .......... .......... .......... 71% 22.9M 6s
190400K .......... .......... .......... .......... .......... 71% 11.8M 6s
190450K .......... .......... .......... .......... .......... 71% 6.01M 6s
190500K .......... .......... .......... .......... .......... 71% 44.7M 6s
190550K .......... .......... .......... .......... .......... 71% 12.8M 6s
190600K .......... .......... .......... .......... .......... 71% 7.11M 6s
190650K .......... .......... .......... .......... .......... 71% 12.1M 6s
190700K .......... .......... .......... .......... .......... 71% 13.0M 6s
190750K .......... .......... .......... .......... .......... 71% 8.73M 6s
190800K .......... .......... .......... .......... .......... 71% 9.68M 6s
190850K .......... .......... .......... .......... .......... 71% 25.3M 6s
190900K .......... .......... .......... .......... .......... 71% 10.5M 6s
190950K .......... .......... .......... .......... .......... 71% 6.83M 6s
191000K .......... .......... .......... .......... .......... 71% 40.3M 6s
191050K .......... .......... .......... .......... .......... 71% 13.1M 6s
191100K .......... .......... .......... .......... .......... 71% 6.07M 6s
191150K .......... .......... .......... .......... .......... 71% 10.8M 6s
191200K .......... .......... .......... .......... .......... 71% 16.7M 6s
191250K .......... .......... .......... .......... .......... 71% 10.1M 6s
191300K .......... .......... .......... .......... .......... 72% 9.46M 6s
191350K .......... .......... .......... .......... .......... 72% 17.6M 6s
191400K .......... .......... .......... .......... .......... 72% 17.8M 6s
191450K .......... .......... .......... .......... .......... 72% 5.80M 6s
191500K .......... .......... .......... .......... .......... 72% 21.8M 6s
191550K .......... .......... .......... .......... .......... 72% 19.5M 6s
191600K .......... .......... .......... .......... .......... 72% 6.00M 6s
191650K .......... .......... .......... .......... .......... 72% 14.6M 6s
191700K .......... .......... .......... .......... .......... 72% 13.2M 6s
191750K .......... .......... .......... .......... .......... 72% 29.2M 6s
191800K .......... .......... .......... .......... .......... 72% 5.45M 6s
191850K .......... .......... .......... .......... .......... 72% 23.5M 6s
191900K .......... .......... .......... .......... .......... 72% 16.8M 6s
191950K .......... .......... .......... .......... .......... 72% 5.76M 6s
192000K .......... .......... .......... .......... .......... 72% 12.8M 6s
192050K .......... .......... .......... .......... .......... 72% 25.2M 6s
192100K .......... .......... .......... .......... .......... 72% 8.52M 6s
192150K .......... .......... .......... .......... .......... 72% 8.47M 6s
192200K .......... .......... .......... .......... .......... 72% 13.7M 6s
192250K .......... .......... .......... .......... .......... 72% 25.3M 6s
192300K .......... .......... .......... .......... .......... 72% 6.83M 6s
192350K .......... .......... .......... .......... .......... 72% 12.7M 6s
192400K .......... .......... .......... .......... .......... 72% 18.2M 6s
192450K .......... .......... .......... .......... .......... 72% 5.85M 6s
192500K .......... .......... .......... .......... .......... 72% 15.1M 5s
192550K .......... .......... .......... .......... .......... 72% 19.1M 5s
192600K .......... .......... .......... .......... .......... 72% 7.93M 5s
192650K .......... .......... .......... .......... .......... 72% 8.88M 5s
192700K .......... .......... .......... .......... .......... 72% 18.2M 5s
192750K .......... .......... .......... .......... .......... 72% 18.1M 5s
192800K .......... .......... .......... .......... .......... 72% 6.52M 5s
192850K .......... .......... .......... .......... .......... 72% 10.3M 5s
192900K .......... .......... .......... .......... .......... 72% 29.6M 5s
192950K .......... .......... .......... .......... .......... 72% 8.94M 5s
193000K .......... .......... .......... .......... .......... 72% 7.68M 5s
193050K .......... .......... .......... .......... .......... 72% 25.5M 5s
193100K .......... .......... .......... .......... .......... 72% 18.0M 5s
193150K .......... .......... .......... .......... .......... 72% 6.53M 5s
193200K .......... .......... .......... .......... .......... 72% 11.0M 5s
193250K .......... .......... .......... .......... .......... 72% 25.2M 5s
193300K .......... .......... .......... .......... .......... 72% 10.2M 5s
193350K .......... .......... .......... .......... .......... 72% 6.83M 5s
193400K .......... .......... .......... .......... .......... 72% 24.8M 5s
193450K .......... .......... .......... .......... .......... 72% 13.5M 5s
193500K .......... .......... .......... .......... .......... 72% 7.85M 5s
193550K .......... .......... .......... .......... .......... 72% 10.9M 5s
193600K .......... .......... .......... .......... .......... 72% 16.9M 5s
193650K .......... .......... .......... .......... .......... 72% 11.4M 5s
193700K .......... .......... .......... .......... .......... 72% 7.87M 5s
193750K .......... .......... .......... .......... .......... 72% 14.3M 5s
193800K .......... .......... .......... .......... .......... 72% 22.9M 5s
193850K .......... .......... .......... .......... .......... 72% 6.78M 5s
193900K .......... .......... .......... .......... .......... 72% 10.6M 5s
193950K .......... .......... .......... .......... .......... 73% 17.2M 5s
194000K .......... .......... .......... .......... .......... 73% 7.01M 5s
194050K .......... .......... .......... .......... .......... 73% 13.0M 5s
194100K .......... .......... .......... .......... .......... 73% 14.0M 5s
194150K .......... .......... .......... .......... .......... 73% 20.9M 5s
194200K .......... .......... .......... .......... .......... 73% 6.24M 5s
194250K .......... .......... .......... .......... .......... 73% 10.7M 5s
194300K .......... .......... .......... .......... .......... 73% 21.9M 5s
194350K .......... .......... .......... .......... .......... 73% 9.99M 5s
194400K .......... .......... .......... .......... .......... 73% 9.46M 5s
194450K .......... .......... .......... .......... .......... 73% 10.4M 5s
194500K .......... .......... .......... .......... .......... 73% 18.9M 5s
194550K .......... .......... .......... .......... .......... 73% 6.80M 5s
194600K .......... .......... .......... .......... .......... 73% 8.67M 5s
194650K .......... .......... .......... .......... .......... 73% 33.9M 5s
194700K .......... .......... .......... .......... .......... 73% 16.3M 5s
194750K .......... .......... .......... .......... .......... 73% 7.12M 5s
194800K .......... .......... .......... .......... .......... 73% 11.6M 5s
194850K .......... .......... .......... .......... .......... 73% 19.4M 5s
194900K .......... .......... .......... .......... .......... 73% 11.6M 5s
194950K .......... .......... .......... .......... .......... 73% 6.57M 5s
195000K .......... .......... .......... .......... .......... 73% 27.2M 5s
195050K .......... .......... .......... .......... .......... 73% 17.9M 5s
195100K .......... .......... .......... .......... .......... 73% 6.68M 5s
195150K .......... .......... .......... .......... .......... 73% 10.1M 5s
195200K .......... .......... .......... .......... .......... 73% 18.0M 5s
195250K .......... .......... .......... .......... .......... 73% 10.6M 5s
195300K .......... .......... .......... .......... .......... 73% 7.85M 5s
195350K .......... .......... .......... .......... .......... 73% 14.6M 5s
195400K .......... .......... .......... .......... .......... 73% 30.3M 5s
195450K .......... .......... .......... .......... .......... 73% 6.59M 5s
195500K .......... .......... .......... .......... .......... 73% 9.16M 5s
195550K .......... .......... .......... .......... .......... 73% 26.3M 5s
195600K .......... .......... .......... .......... .......... 73% 12.0M 5s
195650K .......... .......... .......... .......... .......... 73% 5.19M 5s
195700K .......... .......... .......... .......... .......... 73% 8.54M 5s
195750K .......... .......... .......... .......... .......... 73% 27.3M 5s
195800K .......... .......... .......... .......... .......... 73% 30.0M 5s
195850K .......... .......... .......... .......... .......... 73% 7.85M 5s
195900K .......... .......... .......... .......... .......... 73% 5.56M 5s
195950K .......... .......... .......... .......... .......... 73% 7.76M 5s
196000K .......... .......... .......... .......... .......... 73% 7.72M 5s
196050K .......... .......... .......... .......... .......... 73% 9.88M 5s
196100K .......... .......... .......... .......... .......... 73% 21.3M 5s
196150K .......... .......... .......... .......... .......... 73% 14.6M 5s
196200K .......... .......... .......... .......... .......... 73% 17.2M 5s
196250K .......... .......... .......... .......... .......... 73% 10.5M 5s
196300K .......... .......... .......... .......... .......... 73% 18.2M 5s
196350K .......... .......... .......... .......... .......... 73% 18.8M 5s
196400K .......... .......... .......... .......... .......... 73% 12.1M 5s
196450K .......... .......... .......... .......... .......... 73% 14.5M 5s
196500K .......... .......... .......... .......... .......... 73% 24.6M 5s
196550K .......... .......... .......... .......... .......... 73% 46.3M 5s
196600K .......... .......... .......... .......... .......... 73% 4.46M 5s
196650K .......... .......... .......... .......... .......... 74% 18.8M 5s
196700K .......... .......... .......... .......... .......... 74% 36.6M 5s
196750K .......... .......... .......... .......... .......... 74% 12.4M 5s
196800K .......... .......... .......... .......... .......... 74% 6.08M 5s
196850K .......... .......... .......... .......... .......... 74% 26.2M 5s
196900K .......... .......... .......... .......... .......... 74% 82.7M 5s
196950K .......... .......... .......... .......... .......... 74% 6.14M 5s
197000K .......... .......... .......... .......... .......... 74% 9.15M 5s
197050K .......... .......... .......... .......... .......... 74% 51.6M 5s
197100K .......... .......... .......... .......... .......... 74% 33.1M 5s
197150K .......... .......... .......... .......... .......... 74% 6.93M 5s
197200K .......... .......... .......... .......... .......... 74% 7.95M 5s
197250K .......... .......... .......... .......... .......... 74% 70.2M 5s
197300K .......... .......... .......... .......... .......... 74% 28.2M 5s
197350K .......... .......... .......... .......... .......... 74% 5.51M 5s
197400K .......... .......... .......... .......... .......... 74% 12.1M 5s
197450K .......... .......... .......... .......... .......... 74% 40.7M 5s
197500K .......... .......... .......... .......... .......... 74% 11.2M 5s
197550K .......... .......... .......... .......... .......... 74% 6.35M 5s
197600K .......... .......... .......... .......... .......... 74% 13.8M 5s
197650K .......... .......... .......... .......... .......... 74% 67.9M 5s
197700K .......... .......... .......... .......... .......... 74% 6.28M 5s
197750K .......... .......... .......... .......... .......... 74% 11.8M 5s
197800K .......... .......... .......... .......... .......... 74% 13.3M 5s
197850K .......... .......... .......... .......... .......... 74% 15.9M 5s
197900K .......... .......... .......... .......... .......... 74% 10.4M 5s
197950K .......... .......... .......... .......... .......... 74% 9.15M 5s
198000K .......... .......... .......... .......... .......... 74% 17.8M 5s
198050K .......... .......... .......... .......... .......... 74% 18.8M 5s
198100K .......... .......... .......... .......... .......... 74% 8.35M 5s
198150K .......... .......... .......... .......... .......... 74% 9.80M 5s
198200K .......... .......... .......... .......... .......... 74% 16.8M 5s
198250K .......... .......... .......... .......... .......... 74% 21.5M 5s
198300K .......... .......... .......... .......... .......... 74% 9.01M 5s
198350K .......... .......... .......... .......... .......... 74% 10.4M 5s
198400K .......... .......... .......... .......... .......... 74% 20.1M 5s
198450K .......... .......... .......... .......... .......... 74% 17.9M 5s
198500K .......... .......... .......... .......... .......... 74% 8.81M 5s
198550K .......... .......... .......... .......... .......... 74% 12.3M 5s
198600K .......... .......... .......... .......... .......... 74% 19.3M 5s
198650K .......... .......... .......... .......... .......... 74% 15.6M 5s
198700K .......... .......... .......... .......... .......... 74% 2.84M 5s
198750K .......... .......... .......... .......... .......... 74% 81.3M 5s
198800K .......... .......... .......... .......... .......... 74% 146M 5s
198850K .......... .......... .......... .......... .......... 74% 36.6M 5s
198900K .......... .......... .......... .......... .......... 74% 117M 5s
198950K .......... .......... .......... .......... .......... 74% 14.5M 5s
199000K .......... .......... .......... .......... .......... 74% 16.6M 5s
199050K .......... .......... .......... .......... .......... 74% 8.70M 5s
199100K .......... .......... .......... .......... .......... 74% 13.8M 5s
199150K .......... .......... .......... .......... .......... 74% 11.3M 5s
199200K .......... .......... .......... .......... .......... 74% 9.66M 5s
199250K .......... .......... .......... .......... .......... 74% 27.7M 5s
199300K .......... .......... .......... .......... .......... 75% 6.76M 5s
199350K .......... .......... .......... .......... .......... 75% 15.7M 5s
199400K .......... .......... .......... .......... .......... 75% 17.3M 5s
199450K .......... .......... .......... .......... .......... 75% 7.02M 5s
199500K .......... .......... .......... .......... .......... 75% 15.0M 5s
199550K .......... .......... .......... .......... .......... 75% 26.1M 5s
199600K .......... .......... .......... .......... .......... 75% 9.90M 5s
199650K .......... .......... .......... .......... .......... 75% 14.6M 5s
199700K .......... .......... .......... .......... .......... 75% 12.4M 5s
199750K .......... .......... .......... .......... .......... 75% 11.9M 5s
199800K .......... .......... .......... .......... .......... 75% 29.6M 5s
199850K .......... .......... .......... .......... .......... 75% 12.1M 5s
199900K .......... .......... .......... .......... .......... 75% 18.4M 5s
199950K .......... .......... .......... .......... .......... 75% 14.9M 5s
200000K .......... .......... .......... .......... .......... 75% 14.3M 5s
200050K .......... .......... .......... .......... .......... 75% 20.7M 5s
200100K .......... .......... .......... .......... .......... 75% 18.9M 5s
200150K .......... .......... .......... .......... .......... 75% 10.3M 5s
200200K .......... .......... .......... .......... .......... 75% 18.4M 5s
200250K .......... .......... .......... .......... .......... 75% 31.5M 5s
200300K .......... .......... .......... .......... .......... 75% 12.4M 5s
200350K .......... .......... .......... .......... .......... 75% 27.9M 5s
200400K .......... .......... .......... .......... .......... 75% 17.7M 5s
200450K .......... .......... .......... .......... .......... 75% 10.8M 5s
200500K .......... .......... .......... .......... .......... 75% 22.4M 5s
200550K .......... .......... .......... .......... .......... 75% 22.6M 5s
200600K .......... .......... .......... .......... .......... 75% 11.1M 5s
200650K .......... .......... .......... .......... .......... 75% 24.2M 5s
200700K .......... .......... .......... .......... .......... 75% 15.7M 5s
200750K .......... .......... .......... .......... .......... 75% 15.0M 5s
200800K .......... .......... .......... .......... .......... 75% 24.7M 5s
200850K .......... .......... .......... .......... .......... 75% 9.30M 5s
200900K .......... .......... .......... .......... .......... 75% 29.1M 5s
200950K .......... .......... .......... .......... .......... 75% 28.0M 5s
201000K .......... .......... .......... .......... .......... 75% 8.43M 5s
201050K .......... .......... .......... .......... .......... 75% 46.9M 5s
201100K .......... .......... .......... .......... .......... 75% 12.8M 5s
201150K .......... .......... .......... .......... .......... 75% 14.4M 5s
201200K .......... .......... .......... .......... .......... 75% 29.4M 5s
201250K .......... .......... .......... .......... .......... 75% 17.9M 5s
201300K .......... .......... .......... .......... .......... 75% 10.6M 5s
201350K .......... .......... .......... .......... .......... 75% 21.1M 5s
201400K .......... .......... .......... .......... .......... 75% 20.5M 5s
201450K .......... .......... .......... .......... .......... 75% 9.35M 5s
201500K .......... .......... .......... .......... .......... 75% 33.0M 5s
201550K .......... .......... .......... .......... .......... 75% 27.7M 5s
201600K .......... .......... .......... .......... .......... 75% 10.3M 5s
201650K .......... .......... .......... .......... .......... 75% 27.2M 5s
201700K .......... .......... .......... .......... .......... 75% 4.27M 5s
201750K .......... .......... .......... .......... .......... 75% 33.6M 5s
201800K .......... .......... .......... .......... .......... 75% 171M 5s
201850K .......... .......... .......... .......... .......... 75% 36.3M 5s
201900K .......... .......... .......... .......... .......... 75% 33.2M 5s
201950K .......... .......... .......... .......... .......... 76% 17.4M 5s
202000K .......... .......... .......... .......... .......... 76% 16.5M 5s
202050K .......... .......... .......... .......... .......... 76% 13.6M 5s
202100K .......... .......... .......... .......... .......... 76% 18.5M 5s
202150K .......... .......... .......... .......... .......... 76% 12.7M 5s
202200K .......... .......... .......... .......... .......... 76% 15.1M 5s
202250K .......... .......... .......... .......... .......... 76% 16.3M 5s
202300K .......... .......... .......... .......... .......... 76% 14.6M 5s
202350K .......... .......... .......... .......... .......... 76% 19.8M 5s
202400K .......... .......... .......... .......... .......... 76% 10.9M 5s
202450K .......... .......... .......... .......... .......... 76% 28.5M 5s
202500K .......... .......... .......... .......... .......... 76% 12.2M 5s
202550K .......... .......... .......... .......... .......... 76% 18.7M 5s
202600K .......... .......... .......... .......... .......... 76% 11.0M 5s
202650K .......... .......... .......... .......... .......... 76% 22.8M 5s
202700K .......... .......... .......... .......... .......... 76% 11.0M 5s
202750K .......... .......... .......... .......... .......... 76% 26.6M 5s
202800K .......... .......... .......... .......... .......... 76% 12.8M 5s
202850K .......... .......... .......... .......... .......... 76% 25.5M 5s
202900K .......... .......... .......... .......... .......... 76% 10.4M 5s
202950K .......... .......... .......... .......... .......... 76% 26.0M 5s
203000K .......... .......... .......... .......... .......... 76% 17.3M 5s
203050K .......... .......... .......... .......... .......... 76% 14.8M 5s
203100K .......... .......... .......... .......... .......... 76% 13.5M 5s
203150K .......... .......... .......... .......... .......... 76% 12.5M 5s
203200K .......... .......... .......... .......... .......... 76% 27.3M 5s
203250K .......... .......... .......... .......... .......... 76% 11.9M 5s
203300K .......... .......... .......... .......... .......... 76% 24.0M 5s
203350K .......... .......... .......... .......... .......... 76% 9.68M 5s
203400K .......... .......... .......... .......... .......... 76% 23.9M 5s
203450K .......... .......... .......... .......... .......... 76% 10.2M 5s
203500K .......... .......... .......... .......... .......... 76% 29.8M 5s
203550K .......... .......... .......... .......... .......... 76% 12.4M 5s
203600K .......... .......... .......... .......... .......... 76% 16.9M 5s
203650K .......... .......... .......... .......... .......... 76% 13.5M 5s
203700K .......... .......... .......... .......... .......... 76% 4.61M 5s
203750K .......... .......... .......... .......... .......... 76% 32.3M 5s
203800K .......... .......... .......... .......... .......... 76% 82.3M 5s
203850K .......... .......... .......... .......... .......... 76% 18.3M 5s
203900K .......... .......... .......... .......... .......... 76% 21.2M 5s
203950K .......... .......... .......... .......... .......... 76% 11.6M 5s
204000K .......... .......... .......... .......... .......... 76% 10.6M 5s
204050K .......... .......... .......... .......... .......... 76% 14.6M 5s
204100K .......... .......... .......... .......... .......... 76% 7.21M 5s
204150K .......... .......... .......... .......... .......... 76% 14.7M 5s
204200K .......... .......... .......... .......... .......... 76% 13.9M 5s
204250K .......... .......... .......... .......... .......... 76% 8.16M 5s
204300K .......... .......... .......... .......... .......... 76% 12.4M 5s
204350K .......... .......... .......... .......... .......... 76% 12.5M 5s
204400K .......... .......... .......... .......... .......... 76% 8.51M 5s
204450K .......... .......... .......... .......... .......... 76% 17.8M 5s
204500K .......... .......... .......... .......... .......... 76% 9.19M 5s
204550K .......... .......... .......... .......... .......... 76% 9.98M 5s
204600K .......... .......... .......... .......... .......... 77% 21.0M 5s
204650K .......... .......... .......... .......... .......... 77% 8.26M 5s
204700K .......... .......... .......... .......... .......... 77% 9.77M 5s
204750K .......... .......... .......... .......... .......... 77% 9.74M 5s
204800K .......... .......... .......... .......... .......... 77% 6.38M 5s
204850K .......... .......... .......... .......... .......... 77% 11.5M 5s
204900K .......... .......... .......... .......... .......... 77% 7.95M 5s
204950K .......... .......... .......... .......... .......... 77% 9.58M 5s
205000K .......... .......... .......... .......... .......... 77% 8.75M 5s
205050K .......... .......... .......... .......... .......... 77% 7.35M 5s
205100K .......... .......... .......... .......... .......... 77% 9.98M 5s
205150K .......... .......... .......... .......... .......... 77% 7.49M 5s
205200K .......... .......... .......... .......... .......... 77% 11.3M 5s
205250K .......... .......... .......... .......... .......... 77% 5.87M 5s
205300K .......... .......... .......... .......... .......... 77% 16.9M 5s
205350K .......... .......... .......... .......... .......... 77% 5.75M 5s
205400K .......... .......... .......... .......... .......... 77% 9.37M 5s
205450K .......... .......... .......... .......... .......... 77% 11.2M 5s
205500K .......... .......... .......... .......... .......... 77% 11.1M 5s
205550K .......... .......... .......... .......... .......... 77% 15.0M 5s
205600K .......... .......... .......... .......... .......... 77% 9.81M 5s
205650K .......... .......... .......... .......... .......... 77% 16.7M 5s
205700K .......... .......... .......... .......... .......... 77% 6.52M 5s
205750K .......... .......... .......... .......... .......... 77% 12.5M 5s
205800K .......... .......... .......... .......... .......... 77% 9.41M 5s
205850K .......... .......... .......... .......... .......... 77% 9.36M 5s
205900K .......... .......... .......... .......... .......... 77% 14.3M 5s
205950K .......... .......... .......... .......... .......... 77% 9.91M 5s
206000K .......... .......... .......... .......... .......... 77% 10.7M 5s
206050K .......... .......... .......... .......... .......... 77% 8.40M 4s
206100K .......... .......... .......... .......... .......... 77% 12.0M 4s
206150K .......... .......... .......... .......... .......... 77% 12.3M 4s
206200K .......... .......... .......... .......... .......... 77% 11.1M 4s
206250K .......... .......... .......... .......... .......... 77% 8.17M 4s
206300K .......... .......... .......... .......... .......... 77% 18.4M 4s
206350K .......... .......... .......... .......... .......... 77% 8.27M 4s
206400K .......... .......... .......... .......... .......... 77% 17.9M 4s
206450K .......... .......... .......... .......... .......... 77% 8.80M 4s
206500K .......... .......... .......... .......... .......... 77% 9.26M 4s
206550K .......... .......... .......... .......... .......... 77% 15.4M 4s
206600K .......... .......... .......... .......... .......... 77% 9.54M 4s
206650K .......... .......... .......... .......... .......... 77% 15.8M 4s
206700K .......... .......... .......... .......... .......... 77% 8.04M 4s
206750K .......... .......... .......... .......... .......... 77% 17.8M 4s
206800K .......... .......... .......... .......... .......... 77% 8.99M 4s
206850K .......... .......... .......... .......... .......... 77% 15.8M 4s
206900K .......... .......... .......... .......... .......... 77% 8.71M 4s
206950K .......... .......... .......... .......... .......... 77% 16.9M 4s
207000K .......... .......... .......... .......... .......... 77% 8.10M 4s
207050K .......... .......... .......... .......... .......... 77% 21.4M 4s
207100K .......... .......... .......... .......... .......... 77% 8.16M 4s
207150K .......... .......... .......... .......... .......... 77% 16.9M 4s
207200K .......... .......... .......... .......... .......... 77% 7.86M 4s
207250K .......... .......... .......... .......... .......... 78% 19.4M 4s
207300K .......... .......... .......... .......... .......... 78% 8.43M 4s
207350K .......... .......... .......... .......... .......... 78% 16.4M 4s
207400K .......... .......... .......... .......... .......... 78% 8.26M 4s
207450K .......... .......... .......... .......... .......... 78% 15.8M 4s
207500K .......... .......... .......... .......... .......... 78% 8.19M 4s
207550K .......... .......... .......... .......... .......... 78% 19.3M 4s
207600K .......... .......... .......... .......... .......... 78% 7.07M 4s
207650K .......... .......... .......... .......... .......... 78% 23.1M 4s
207700K .......... .......... .......... .......... .......... 78% 7.49M 4s
207750K .......... .......... .......... .......... .......... 78% 19.4M 4s
207800K .......... .......... .......... .......... .......... 78% 7.41M 4s
207850K .......... .......... .......... .......... .......... 78% 16.2M 4s
207900K .......... .......... .......... .......... .......... 78% 8.81M 4s
207950K .......... .......... .......... .......... .......... 78% 20.5M 4s
208000K .......... .......... .......... .......... .......... 78% 10.6M 4s
208050K .......... .......... .......... .......... .......... 78% 11.4M 4s
208100K .......... .......... .......... .......... .......... 78% 8.47M 4s
208150K .......... .......... .......... .......... .......... 78% 11.8M 4s
208200K .......... .......... .......... .......... .......... 78% 13.0M 4s
208250K .......... .......... .......... .......... .......... 78% 11.9M 4s
208300K .......... .......... .......... .......... .......... 78% 13.7M 4s
208350K .......... .......... .......... .......... .......... 78% 8.23M 4s
208400K .......... .......... .......... .......... .......... 78% 15.6M 4s
208450K .......... .......... .......... .......... .......... 78% 9.34M 4s
208500K .......... .......... .......... .......... .......... 78% 12.1M 4s
208550K .......... .......... .......... .......... .......... 78% 9.92M 4s
208600K .......... .......... .......... .......... .......... 78% 11.3M 4s
208650K .......... .......... .......... .......... .......... 78% 20.4M 4s
208700K .......... .......... .......... .......... .......... 78% 8.81M 4s
208750K .......... .......... .......... .......... .......... 78% 17.1M 4s
208800K .......... .......... .......... .......... .......... 78% 7.04M 4s
208850K .......... .......... .......... .......... .......... 78% 16.2M 4s
208900K .......... .......... .......... .......... .......... 78% 11.7M 4s
208950K .......... .......... .......... .......... .......... 78% 10.2M 4s
209000K .......... .......... .......... .......... .......... 78% 9.45M 4s
209050K .......... .......... .......... .......... .......... 78% 16.7M 4s
209100K .......... .......... .......... .......... .......... 78% 15.9M 4s
209150K .......... .......... .......... .......... .......... 78% 8.01M 4s
209200K .......... .......... .......... .......... .......... 78% 15.4M 4s
209250K .......... .......... .......... .......... .......... 78% 7.13M 4s
209300K .......... .......... .......... .......... .......... 78% 18.1M 4s
209350K .......... .......... .......... .......... .......... 78% 10.9M 4s
209400K .......... .......... .......... .......... .......... 78% 12.5M 4s
209450K .......... .......... .......... .......... .......... 78% 12.3M 4s
209500K .......... .......... .......... .......... .......... 78% 9.89M 4s
209550K .......... .......... .......... .......... .......... 78% 13.5M 4s
209600K .......... .......... .......... .......... .......... 78% 7.54M 4s
209650K .......... .......... .......... .......... .......... 78% 14.0M 4s
209700K .......... .......... .......... .......... .......... 78% 12.8M 4s
209750K .......... .......... .......... .......... .......... 78% 10.7M 4s
209800K .......... .......... .......... .......... .......... 78% 13.9M 4s
209850K .......... .......... .......... .......... .......... 78% 8.85M 4s
209900K .......... .......... .......... .......... .......... 79% 13.1M 4s
209950K .......... .......... .......... .......... .......... 79% 8.09M 4s
210000K .......... .......... .......... .......... .......... 79% 14.5M 4s
210050K .......... .......... .......... .......... .......... 79% 11.4M 4s
210100K .......... .......... .......... .......... .......... 79% 9.87M 4s
210150K .......... .......... .......... .......... .......... 79% 9.50M 4s
210200K .......... .......... .......... .......... .......... 79% 11.1M 4s
210250K .......... .......... .......... .......... .......... 79% 13.1M 4s
210300K .......... .......... .......... .......... .......... 79% 14.1M 4s
210350K .......... .......... .......... .......... .......... 79% 8.74M 4s
210400K .......... .......... .......... .......... .......... 79% 11.2M 4s
210450K .......... .......... .......... .......... .......... 79% 9.98M 4s
210500K .......... .......... .......... .......... .......... 79% 12.6M 4s
210550K .......... .......... .......... .......... .......... 79% 17.2M 4s
210600K .......... .......... .......... .......... .......... 79% 7.73M 4s
210650K .......... .......... .......... .......... .......... 79% 17.0M 4s
210700K .......... .......... .......... .......... .......... 79% 9.51M 4s
210750K .......... .......... .......... .......... .......... 79% 14.9M 4s
210800K .......... .......... .......... .......... .......... 79% 14.0M 4s
210850K .......... .......... .......... .......... .......... 79% 10.9M 4s
210900K .......... .......... .......... .......... .......... 79% 8.64M 4s
210950K .......... .......... .......... .......... .......... 79% 13.0M 4s
211000K .......... .......... .......... .......... .......... 79% 10.2M 4s
211050K .......... .......... .......... .......... .......... 79% 29.3M 4s
211100K .......... .......... .......... .......... .......... 79% 11.1M 4s
211150K .......... .......... .......... .......... .......... 79% 9.38M 4s
211200K .......... .......... .......... .......... .......... 79% 10.2M 4s
211250K .......... .......... .......... .......... .......... 79% 10.9M 4s
211300K .......... .......... .......... .......... .......... 79% 42.6M 4s
211350K .......... .......... .......... .......... .......... 79% 11.2M 4s
211400K .......... .......... .......... .......... .......... 79% 10.5M 4s
211450K .......... .......... .......... .......... .......... 79% 15.0M 4s
211500K .......... .......... .......... .......... .......... 79% 10.5M 4s
211550K .......... .......... .......... .......... .......... 79% 27.5M 4s
211600K .......... .......... .......... .......... .......... 79% 13.0M 4s
211650K .......... .......... .......... .......... .......... 79% 12.7M 4s
211700K .......... .......... .......... .......... .......... 79% 15.8M 4s
211750K .......... .......... .......... .......... .......... 79% 13.8M 4s
211800K .......... .......... .......... .......... .......... 79% 12.7M 4s
211850K .......... .......... .......... .......... .......... 79% 11.3M 4s
211900K .......... .......... .......... .......... .......... 79% 13.7M 4s
211950K .......... .......... .......... .......... .......... 79% 15.1M 4s
212000K .......... .......... .......... .......... .......... 79% 15.0M 4s
212050K .......... .......... .......... .......... .......... 79% 10.3M 4s
212100K .......... .......... .......... .......... .......... 79% 20.5M 4s
212150K .......... .......... .......... .......... .......... 79% 11.8M 4s
212200K .......... .......... .......... .......... .......... 79% 16.1M 4s
212250K .......... .......... .......... .......... .......... 79% 12.3M 4s
212300K .......... .......... .......... .......... .......... 79% 11.4M 4s
212350K .......... .......... .......... .......... .......... 79% 17.7M 4s
212400K .......... .......... .......... .......... .......... 79% 13.1M 4s
212450K .......... .......... .......... .......... .......... 79% 16.7M 4s
212500K .......... .......... .......... .......... .......... 79% 12.5M 4s
212550K .......... .......... .......... .......... .......... 80% 9.56M 4s
212600K .......... .......... .......... .......... .......... 80% 18.1M 4s
212650K .......... .......... .......... .......... .......... 80% 12.6M 4s
212700K .......... .......... .......... .......... .......... 80% 16.8M 4s
212750K .......... .......... .......... .......... .......... 80% 11.0M 4s
212800K .......... .......... .......... .......... .......... 80% 11.9M 4s
212850K .......... .......... .......... .......... .......... 80% 24.2M 4s
212900K .......... .......... .......... .......... .......... 80% 10.9M 4s
212950K .......... .......... .......... .......... .......... 80% 12.7M 4s
213000K .......... .......... .......... .......... .......... 80% 18.1M 4s
213050K .......... .......... .......... .......... .......... 80% 11.1M 4s
213100K .......... .......... .......... .......... .......... 80% 12.3M 4s
213150K .......... .......... .......... .......... .......... 80% 15.4M 4s
213200K .......... .......... .......... .......... .......... 80% 12.7M 4s
213250K .......... .......... .......... .......... .......... 80% 14.1M 4s
213300K .......... .......... .......... .......... .......... 80% 12.1M 4s
213350K .......... .......... .......... .......... .......... 80% 15.1M 4s
213400K .......... .......... .......... .......... .......... 80% 19.4M 4s
213450K .......... .......... .......... .......... .......... 80% 10.0M 4s
213500K .......... .......... .......... .......... .......... 80% 15.8M 4s
213550K .......... .......... .......... .......... .......... 80% 21.4M 4s
213600K .......... .......... .......... .......... .......... 80% 10.4M 4s
213650K .......... .......... .......... .......... .......... 80% 14.6M 4s
213700K .......... .......... .......... .......... .......... 80% 11.3M 4s
213750K .......... .......... .......... .......... .......... 80% 18.2M 4s
213800K .......... .......... .......... .......... .......... 80% 11.3M 4s
213850K .......... .......... .......... .......... .......... 80% 11.7M 4s
213900K .......... .......... .......... .......... .......... 80% 16.7M 4s
213950K .......... .......... .......... .......... .......... 80% 15.2M 4s
214000K .......... .......... .......... .......... .......... 80% 12.9M 4s
214050K .......... .......... .......... .......... .......... 80% 17.1M 4s
214100K .......... .......... .......... .......... .......... 80% 19.3M 4s
214150K .......... .......... .......... .......... .......... 80% 12.6M 4s
214200K .......... .......... .......... .......... .......... 80% 19.6M 4s
214250K .......... .......... .......... .......... .......... 80% 9.89M 4s
214300K .......... .......... .......... .......... .......... 80% 35.3M 4s
214350K .......... .......... .......... .......... .......... 80% 13.6M 4s
214400K .......... .......... .......... .......... .......... 80% 11.8M 4s
214450K .......... .......... .......... .......... .......... 80% 22.9M 4s
214500K .......... .......... .......... .......... .......... 80% 13.1M 4s
214550K .......... .......... .......... .......... .......... 80% 14.5M 4s
214600K .......... .......... .......... .......... .......... 80% 20.8M 4s
214650K .......... .......... .......... .......... .......... 80% 17.2M 4s
214700K .......... .......... .......... .......... .......... 80% 10.9M 4s
214750K .......... .......... .......... .......... .......... 80% 28.5M 4s
214800K .......... .......... .......... .......... .......... 80% 13.4M 4s
214850K .......... .......... .......... .......... .......... 80% 12.8M 4s
214900K .......... .......... .......... .......... .......... 80% 49.2M 4s
214950K .......... .......... .......... .......... .......... 80% 11.4M 4s
215000K .......... .......... .......... .......... .......... 80% 11.7M 4s
215050K .......... .......... .......... .......... .......... 80% 20.6M 4s
215100K .......... .......... .......... .......... .......... 80% 18.4M 4s
215150K .......... .......... .......... .......... .......... 80% 10.8M 4s
215200K .......... .......... .......... .......... .......... 80% 12.3M 4s
215250K .......... .......... .......... .......... .......... 81% 93.6M 4s
215300K .......... .......... .......... .......... .......... 81% 11.3M 4s
215350K .......... .......... .......... .......... .......... 81% 16.6M 4s
215400K .......... .......... .......... .......... .......... 81% 21.1M 4s
215450K .......... .......... .......... .......... .......... 81% 10.7M 4s
215500K .......... .......... .......... .......... .......... 81% 19.4M 4s
215550K .......... .......... .......... .......... .......... 81% 20.2M 4s
215600K .......... .......... .......... .......... .......... 81% 10.6M 4s
215650K .......... .......... .......... .......... .......... 81% 21.6M 4s
215700K .......... .......... .......... .......... .......... 81% 17.6M 4s
215750K .......... .......... .......... .......... .......... 81% 10.7M 4s
215800K .......... .......... .......... .......... .......... 81% 18.1M 4s
215850K .......... .......... .......... .......... .......... 81% 14.1M 4s
215900K .......... .......... .......... .......... .......... 81% 15.2M 4s
215950K .......... .......... .......... .......... .......... 81% 15.7M 4s
216000K .......... .......... .......... .......... .......... 81% 19.8M 4s
216050K .......... .......... .......... .......... .......... 81% 12.8M 4s
216100K .......... .......... .......... .......... .......... 81% 16.7M 4s
216150K .......... .......... .......... .......... .......... 81% 30.0M 4s
216200K .......... .......... .......... .......... .......... 81% 11.0M 4s
216250K .......... .......... .......... .......... .......... 81% 16.1M 4s
216300K .......... .......... .......... .......... .......... 81% 36.0M 4s
216350K .......... .......... .......... .......... .......... 81% 10.3M 4s
216400K .......... .......... .......... .......... .......... 81% 16.4M 4s
216450K .......... .......... .......... .......... .......... 81% 13.4M 4s
216500K .......... .......... .......... .......... .......... 81% 22.8M 4s
216550K .......... .......... .......... .......... .......... 81% 13.5M 4s
216600K .......... .......... .......... .......... .......... 81% 31.8M 4s
216650K .......... .......... .......... .......... .......... 81% 13.3M 4s
216700K .......... .......... .......... .......... .......... 81% 14.4M 4s
216750K .......... .......... .......... .......... .......... 81% 14.1M 4s
216800K .......... .......... .......... .......... .......... 81% 24.9M 4s
216850K .......... .......... .......... .......... .......... 81% 16.1M 4s
216900K .......... .......... .......... .......... .......... 81% 13.3M 4s
216950K .......... .......... .......... .......... .......... 81% 25.9M 4s
217000K .......... .......... .......... .......... .......... 81% 30.7M 4s
217050K .......... .......... .......... .......... .......... 81% 12.5M 4s
217100K .......... .......... .......... .......... .......... 81% 14.0M 4s
217150K .......... .......... .......... .......... .......... 81% 30.0M 4s
217200K .......... .......... .......... .......... .......... 81% 7.77M 4s
217250K .......... .......... .......... .......... .......... 81% 24.1M 4s
217300K .......... .......... .......... .......... .......... 81% 30.5M 4s
217350K .......... .......... .......... .......... .......... 81% 12.0M 4s
217400K .......... .......... .......... .......... .......... 81% 12.9M 4s
217450K .......... .......... .......... .......... .......... 81% 12.9M 4s
217500K .......... .......... .......... .......... .......... 81% 19.5M 4s
217550K .......... .......... .......... .......... .......... 81% 12.3M 4s
217600K .......... .......... .......... .......... .......... 81% 13.6M 4s
217650K .......... .......... .......... .......... .......... 81% 27.8M 4s
217700K .......... .......... .......... .......... .......... 81% 11.9M 4s
217750K .......... .......... .......... .......... .......... 81% 33.1M 4s
217800K .......... .......... .......... .......... .......... 81% 18.7M 4s
217850K .......... .......... .......... .......... .......... 81% 11.0M 4s
217900K .......... .......... .......... .......... .......... 82% 17.9M 4s
217950K .......... .......... .......... .......... .......... 82% 17.4M 4s
218000K .......... .......... .......... .......... .......... 82% 15.4M 4s
218050K .......... .......... .......... .......... .......... 82% 16.2M 4s
218100K .......... .......... .......... .......... .......... 82% 15.4M 4s
218150K .......... .......... .......... .......... .......... 82% 15.3M 4s
218200K .......... .......... .......... .......... .......... 82% 14.5M 4s
218250K .......... .......... .......... .......... .......... 82% 16.6M 4s
218300K .......... .......... .......... .......... .......... 82% 13.7M 4s
218350K .......... .......... .......... .......... .......... 82% 19.9M 4s
218400K .......... .......... .......... .......... .......... 82% 14.7M 4s
218450K .......... .......... .......... .......... .......... 82% 36.4M 4s
218500K .......... .......... .......... .......... .......... 82% 12.3M 4s
218550K .......... .......... .......... .......... .......... 82% 12.0M 4s
218600K .......... .......... .......... .......... .......... 82% 26.1M 4s
218650K .......... .......... .......... .......... .......... 82% 14.3M 4s
218700K .......... .......... .......... .......... .......... 82% 22.3M 4s
218750K .......... .......... .......... .......... .......... 82% 16.3M 4s
218800K .......... .......... .......... .......... .......... 82% 11.9M 4s
218850K .......... .......... .......... .......... .......... 82% 20.1M 4s
218900K .......... .......... .......... .......... .......... 82% 16.5M 4s
218950K .......... .......... .......... .......... .......... 82% 14.2M 4s
219000K .......... .......... .......... .......... .......... 82% 15.9M 4s
219050K .......... .......... .......... .......... .......... 82% 15.0M 4s
219100K .......... .......... .......... .......... .......... 82% 17.5M 4s
219150K .......... .......... .......... .......... .......... 82% 14.8M 4s
219200K .......... .......... .......... .......... .......... 82% 13.5M 4s
219250K .......... .......... .......... .......... .......... 82% 14.8M 3s
219300K .......... .......... .......... .......... .......... 82% 18.2M 3s
219350K .......... .......... .......... .......... .......... 82% 12.5M 3s
219400K .......... .......... .......... .......... .......... 82% 30.4M 3s
219450K .......... .......... .......... .......... .......... 82% 10.8M 3s
219500K .......... .......... .......... .......... .......... 82% 47.0M 3s
219550K .......... .......... .......... .......... .......... 82% 13.9M 3s
219600K .......... .......... .......... .......... .......... 82% 18.2M 3s
219650K .......... .......... .......... .......... .......... 82% 12.9M 3s
219700K .......... .......... .......... .......... .......... 82% 13.4M 3s
219750K .......... .......... .......... .......... .......... 82% 22.8M 3s
219800K .......... .......... .......... .......... .......... 82% 13.7M 3s
219850K .......... .......... .......... .......... .......... 82% 42.7M 3s
219900K .......... .......... .......... .......... .......... 82% 10.4M 3s
219950K .......... .......... .......... .......... .......... 82% 31.3M 3s
220000K .......... .......... .......... .......... .......... 82% 13.0M 3s
220050K .......... .......... .......... .......... .......... 82% 13.9M 3s
220100K .......... .......... .......... .......... .......... 82% 19.7M 3s
220150K .......... .......... .......... .......... .......... 82% 11.9M 3s
220200K .......... .......... .......... .......... .......... 82% 19.0M 3s
220250K .......... .......... .......... .......... .......... 82% 14.0M 3s
220300K .......... .......... .......... .......... .......... 82% 63.8M 3s
220350K .......... .......... .......... .......... .......... 82% 12.0M 3s
220400K .......... .......... .......... .......... .......... 82% 10.9M 3s
220450K .......... .......... .......... .......... .......... 82% 24.2M 3s
220500K .......... .......... .......... .......... .......... 82% 12.4M 3s
220550K .......... .......... .......... .......... .......... 83% 21.7M 3s
220600K .......... .......... .......... .......... .......... 83% 12.8M 3s
220650K .......... .......... .......... .......... .......... 83% 13.2M 3s
220700K .......... .......... .......... .......... .......... 83% 20.4M 3s
220750K .......... .......... .......... .......... .......... 83% 13.9M 3s
220800K .......... .......... .......... .......... .......... 83% 30.3M 3s
220850K .......... .......... .......... .......... .......... 83% 13.6M 3s
220900K .......... .......... .......... .......... .......... 83% 17.7M 3s
220950K .......... .......... .......... .......... .......... 83% 11.3M 3s
221000K .......... .......... .......... .......... .......... 83% 13.6M 3s
221050K .......... .......... .......... .......... .......... 83% 30.9M 3s
221100K .......... .......... .......... .......... .......... 83% 14.0M 3s
221150K .......... .......... .......... .......... .......... 83% 19.9M 3s
221200K .......... .......... .......... .......... .......... 83% 15.1M 3s
221250K .......... .......... .......... .......... .......... 83% 15.3M 3s
221300K .......... .......... .......... .......... .......... 83% 11.5M 3s
221350K .......... .......... .......... .......... .......... 83% 14.2M 3s
221400K .......... .......... .......... .......... .......... 83% 27.5M 3s
221450K .......... .......... .......... .......... .......... 83% 12.6M 3s
221500K .......... .......... .......... .......... .......... 83% 23.6M 3s
221550K .......... .......... .......... .......... .......... 83% 15.9M 3s
221600K .......... .......... .......... .......... .......... 83% 10.4M 3s
221650K .......... .......... .......... .......... .......... 83% 26.3M 3s
221700K .......... .......... .......... .......... .......... 83% 11.2M 3s
221750K .......... .......... .......... .......... .......... 83% 26.8M 3s
221800K .......... .......... .......... .......... .......... 83% 15.6M 3s
221850K .......... .......... .......... .......... .......... 83% 14.2M 3s
221900K .......... .......... .......... .......... .......... 83% 18.9M 3s
221950K .......... .......... .......... .......... .......... 83% 11.2M 3s
222000K .......... .......... .......... .......... .......... 83% 22.5M 3s
222050K .......... .......... .......... .......... .......... 83% 12.6M 3s
222100K .......... .......... .......... .......... .......... 83% 20.1M 3s
222150K .......... .......... .......... .......... .......... 83% 16.1M 3s
222200K .......... .......... .......... .......... .......... 83% 11.0M 3s
222250K .......... .......... .......... .......... .......... 83% 28.4M 3s
222300K .......... .......... .......... .......... .......... 83% 16.4M 3s
222350K .......... .......... .......... .......... .......... 83% 12.7M 3s
222400K .......... .......... .......... .......... .......... 83% 12.3M 3s
222450K .......... .......... .......... .......... .......... 83% 21.7M 3s
222500K .......... .......... .......... .......... .......... 83% 15.4M 3s
222550K .......... .......... .......... .......... .......... 83% 14.7M 3s
222600K .......... .......... .......... .......... .......... 83% 10.9M 3s
222650K .......... .......... .......... .......... .......... 83% 17.5M 3s
222700K .......... .......... .......... .......... .......... 83% 23.8M 3s
222750K .......... .......... .......... .......... .......... 83% 12.2M 3s
222800K .......... .......... .......... .......... .......... 83% 19.8M 3s
222850K .......... .......... .......... .......... .......... 83% 16.6M 3s
222900K .......... .......... .......... .......... .......... 83% 11.8M 3s
222950K .......... .......... .......... .......... .......... 83% 11.0M 3s
223000K .......... .......... .......... .......... .......... 83% 19.6M 3s
223050K .......... .......... .......... .......... .......... 83% 16.2M 3s
223100K .......... .......... .......... .......... .......... 83% 11.2M 3s
223150K .......... .......... .......... .......... .......... 83% 17.6M 3s
223200K .......... .......... .......... .......... .......... 84% 16.9M 3s
223250K .......... .......... .......... .......... .......... 84% 16.1M 3s
223300K .......... .......... .......... .......... .......... 84% 10.8M 3s
223350K .......... .......... .......... .......... .......... 84% 28.1M 3s
223400K .......... .......... .......... .......... .......... 84% 14.9M 3s
223450K .......... .......... .......... .......... .......... 84% 12.1M 3s
223500K .......... .......... .......... .......... .......... 84% 14.0M 3s
223550K .......... .......... .......... .......... .......... 84% 23.8M 3s
223600K .......... .......... .......... .......... .......... 84% 12.5M 3s
223650K .......... .......... .......... .......... .......... 84% 13.4M 3s
223700K .......... .......... .......... .......... .......... 84% 16.4M 3s
223750K .......... .......... .......... .......... .......... 84% 14.4M 3s
223800K .......... .......... .......... .......... .......... 84% 13.8M 3s
223850K .......... .......... .......... .......... .......... 84% 12.2M 3s
223900K .......... .......... .......... .......... .......... 84% 22.4M 3s
223950K .......... .......... .......... .......... .......... 84% 24.1M 3s
224000K .......... .......... .......... .......... .......... 84% 9.14M 3s
224050K .......... .......... .......... .......... .......... 84% 18.5M 3s
224100K .......... .......... .......... .......... .......... 84% 18.0M 3s
224150K .......... .......... .......... .......... .......... 84% 21.3M 3s
224200K .......... .......... .......... .......... .......... 84% 9.55M 3s
224250K .......... .......... .......... .......... .......... 84% 22.0M 3s
224300K .......... .......... .......... .......... .......... 84% 21.0M 3s
224350K .......... .......... .......... .......... .......... 84% 12.3M 3s
224400K .......... .......... .......... .......... .......... 84% 12.1M 3s
224450K .......... .......... .......... .......... .......... 84% 21.1M 3s
224500K .......... .......... .......... .......... .......... 84% 22.6M 3s
224550K .......... .......... .......... .......... .......... 84% 22.0M 3s
224600K .......... .......... .......... .......... .......... 84% 7.09M 3s
224650K .......... .......... .......... .......... .......... 84% 29.5M 3s
224700K .......... .......... .......... .......... .......... 84% 26.6M 3s
224750K .......... .......... .......... .......... .......... 84% 9.66M 3s
224800K .......... .......... .......... .......... .......... 84% 13.9M 3s
224850K .......... .......... .......... .......... .......... 84% 32.4M 3s
224900K .......... .......... .......... .......... .......... 84% 18.6M 3s
224950K .......... .......... .......... .......... .......... 84% 8.08M 3s
225000K .......... .......... .......... .......... .......... 84% 31.9M 3s
225050K .......... .......... .......... .......... .......... 84% 27.1M 3s
225100K .......... .......... .......... .......... .......... 84% 16.5M 3s
225150K .......... .......... .......... .......... .......... 84% 8.05M 3s
225200K .......... .......... .......... .......... .......... 84% 40.4M 3s
225250K .......... .......... .......... .......... .......... 84% 22.1M 3s
225300K .......... .......... .......... .......... .......... 84% 23.3M 3s
225350K .......... .......... .......... .......... .......... 84% 6.23M 3s
225400K .......... .......... .......... .......... .......... 84% 49.7M 3s
225450K .......... .......... .......... .......... .......... 84% 19.5M 3s
225500K .......... .......... .......... .......... .......... 84% 21.0M 3s
225550K .......... .......... .......... .......... .......... 84% 7.95M 3s
225600K .......... .......... .......... .......... .......... 84% 13.5M 3s
225650K .......... .......... .......... .......... .......... 84% 14.2M 3s
225700K .......... .......... .......... .......... .......... 84% 13.4M 3s
225750K .......... .......... .......... .......... .......... 84% 14.3M 3s
225800K .......... .......... .......... .......... .......... 84% 31.8M 3s
225850K .......... .......... .......... .......... .......... 85% 8.13M 3s
225900K .......... .......... .......... .......... .......... 85% 12.8M 3s
225950K .......... .......... .......... .......... .......... 85% 20.4M 3s
226000K .......... .......... .......... .......... .......... 85% 24.5M 3s
226050K .......... .......... .......... .......... .......... 85% 19.2M 3s
226100K .......... .......... .......... .......... .......... 85% 8.41M 3s
226150K .......... .......... .......... .......... .......... 85% 48.9M 3s
226200K .......... .......... .......... .......... .......... 85% 21.6M 3s
226250K .......... .......... .......... .......... .......... 85% 19.5M 3s
226300K .......... .......... .......... .......... .......... 85% 8.76M 3s
226350K .......... .......... .......... .......... .......... 85% 30.5M 3s
226400K .......... .......... .......... .......... .......... 85% 29.6M 3s
226450K .......... .......... .......... .......... .......... 85% 8.06M 3s
226500K .......... .......... .......... .......... .......... 85% 18.0M 3s
226550K .......... .......... .......... .......... .......... 85% 35.9M 3s
226600K .......... .......... .......... .......... .......... 85% 16.7M 3s
226650K .......... .......... .......... .......... .......... 85% 12.5M 3s
226700K .......... .......... .......... .......... .......... 85% 12.7M 3s
226750K .......... .......... .......... .......... .......... 85% 38.2M 3s
226800K .......... .......... .......... .......... .......... 85% 35.7M 3s
226850K .......... .......... .......... .......... .......... 85% 10.0M 3s
226900K .......... .......... .......... .......... .......... 85% 17.6M 3s
226950K .......... .......... .......... .......... .......... 85% 30.3M 3s
227000K .......... .......... .......... .......... .......... 85% 19.0M 3s
227050K .......... .......... .......... .......... .......... 85% 13.3M 3s
227100K .......... .......... .......... .......... .......... 85% 15.0M 3s
227150K .......... .......... .......... .......... .......... 85% 27.2M 3s
227200K .......... .......... .......... .......... .......... 85% 20.2M 3s
227250K .......... .......... .......... .......... .......... 85% 10.6M 3s
227300K .......... .......... .......... .......... .......... 85% 26.7M 3s
227350K .......... .......... .......... .......... .......... 85% 18.6M 3s
227400K .......... .......... .......... .......... .......... 85% 26.5M 3s
227450K .......... .......... .......... .......... .......... 85% 9.72M 3s
227500K .......... .......... .......... .......... .......... 85% 25.8M 3s
227550K .......... .......... .......... .......... .......... 85% 16.7M 3s
227600K .......... .......... .......... .......... .......... 85% 15.0M 3s
227650K .......... .......... .......... .......... .......... 85% 13.3M 3s
227700K .......... .......... .......... .......... .......... 85% 3.74M 3s
227750K .......... .......... .......... .......... .......... 85% 35.7M 3s
227800K .......... .......... .......... .......... .......... 85% 104M 3s
227850K .......... .......... .......... .......... .......... 85% 111M 3s
227900K .......... .......... .......... .......... .......... 85% 139M 3s
227950K .......... .......... .......... .......... .......... 85% 9.30M 3s
228000K .......... .......... .......... .......... .......... 85% 27.9M 3s
228050K .......... .......... .......... .......... .......... 85% 19.8M 3s
228100K .......... .......... .......... .......... .......... 85% 8.44M 3s
228150K .......... .......... .......... .......... .......... 85% 19.3M 3s
228200K .......... .......... .......... .......... .......... 85% 10.2M 3s
228250K .......... .......... .......... .......... .......... 85% 11.3M 3s
228300K .......... .......... .......... .......... .......... 85% 28.9M 3s
228350K .......... .......... .......... .......... .......... 85% 9.94M 3s
228400K .......... .......... .......... .......... .......... 85% 10.6M 3s
228450K .......... .......... .......... .......... .......... 85% 37.7M 3s
228500K .......... .......... .......... .......... .......... 86% 9.30M 3s
228550K .......... .......... .......... .......... .......... 86% 12.3M 3s
228600K .......... .......... .......... .......... .......... 86% 35.8M 3s
228650K .......... .......... .......... .......... .......... 86% 8.87M 3s
228700K .......... .......... .......... .......... .......... 86% 9.76M 3s
228750K .......... .......... .......... .......... .......... 86% 30.2M 3s
228800K .......... .......... .......... .......... .......... 86% 7.88M 3s
228850K .......... .......... .......... .......... .......... 86% 19.5M 3s
228900K .......... .......... .......... .......... .......... 86% 18.6M 3s
228950K .......... .......... .......... .......... .......... 86% 10.1M 3s
229000K .......... .......... .......... .......... .......... 86% 50.1M 3s
229050K .......... .......... .......... .......... .......... 86% 29.2M 3s
229100K .......... .......... .......... .......... .......... 86% 10.4M 3s
229150K .......... .......... .......... .......... .......... 86% 22.2M 3s
229200K .......... .......... .......... .......... .......... 86% 16.4M 3s
229250K .......... .......... .......... .......... .......... 86% 12.8M 3s
229300K .......... .......... .......... .......... .......... 86% 24.3M 3s
229350K .......... .......... .......... .......... .......... 86% 18.2M 3s
229400K .......... .......... .......... .......... .......... 86% 14.6M 3s
229450K .......... .......... .......... .......... .......... 86% 20.3M 3s
229500K .......... .......... .......... .......... .......... 86% 19.6M 3s
229550K .......... .......... .......... .......... .......... 86% 14.4M 3s
229600K .......... .......... .......... .......... .......... 86% 20.9M 3s
229650K .......... .......... .......... .......... .......... 86% 17.5M 3s
229700K .......... .......... .......... .......... .......... 86% 9.78M 3s
229750K .......... .......... .......... .......... .......... 86% 20.6M 3s
229800K .......... .......... .......... .......... .......... 86% 30.2M 3s
229850K .......... .......... .......... .......... .......... 86% 8.95M 3s
229900K .......... .......... .......... .......... .......... 86% 36.7M 3s
229950K .......... .......... .......... .......... .......... 86% 18.9M 3s
230000K .......... .......... .......... .......... .......... 86% 12.9M 3s
230050K .......... .......... .......... .......... .......... 86% 28.2M 3s
230100K .......... .......... .......... .......... .......... 86% 17.7M 3s
230150K .......... .......... .......... .......... .......... 86% 13.4M 3s
230200K .......... .......... .......... .......... .......... 86% 24.5M 3s
230250K .......... .......... .......... .......... .......... 86% 23.8M 3s
230300K .......... .......... .......... .......... .......... 86% 13.7M 3s
230350K .......... .......... .......... .......... .......... 86% 18.6M 3s
230400K .......... .......... .......... .......... .......... 86% 35.9M 3s
230450K .......... .......... .......... .......... .......... 86% 12.4M 3s
230500K .......... .......... .......... .......... .......... 86% 19.9M 3s
230550K .......... .......... .......... .......... .......... 86% 22.6M 3s
230600K .......... .......... .......... .......... .......... 86% 15.6M 3s
230650K .......... .......... .......... .......... .......... 86% 18.8M 3s
230700K .......... .......... .......... .......... .......... 86% 17.4M 3s
230750K .......... .......... .......... .......... .......... 86% 23.6M 3s
230800K .......... .......... .......... .......... .......... 86% 20.1M 3s
230850K .......... .......... .......... .......... .......... 86% 14.5M 3s
230900K .......... .......... .......... .......... .......... 86% 22.4M 3s
230950K .......... .......... .......... .......... .......... 86% 25.6M 3s
231000K .......... .......... .......... .......... .......... 86% 14.5M 3s
231050K .......... .......... .......... .......... .......... 86% 20.9M 3s
231100K .......... .......... .......... .......... .......... 86% 18.3M 3s
231150K .......... .......... .......... .......... .......... 87% 15.4M 3s
231200K .......... .......... .......... .......... .......... 87% 26.6M 3s
231250K .......... .......... .......... .......... .......... 87% 17.1M 3s
231300K .......... .......... .......... .......... .......... 87% 16.0M 3s
231350K .......... .......... .......... .......... .......... 87% 23.8M 3s
231400K .......... .......... .......... .......... .......... 87% 15.1M 3s
231450K .......... .......... .......... .......... .......... 87% 19.0M 3s
231500K .......... .......... .......... .......... .......... 87% 24.0M 3s
231550K .......... .......... .......... .......... .......... 87% 19.1M 3s
231600K .......... .......... .......... .......... .......... 87% 11.6M 3s
231650K .......... .......... .......... .......... .......... 87% 43.8M 3s
231700K .......... .......... .......... .......... .......... 87% 17.7M 3s
231750K .......... .......... .......... .......... .......... 87% 17.0M 3s
231800K .......... .......... .......... .......... .......... 87% 22.8M 3s
231850K .......... .......... .......... .......... .......... 87% 3.69M 3s
231900K .......... .......... .......... .......... .......... 87% 40.6M 3s
231950K .......... .......... .......... .......... .......... 87% 155M 3s
232000K .......... .......... .......... .......... .......... 87% 231M 3s
232050K .......... .......... .......... .......... .......... 87% 8.01M 3s
232100K .......... .......... .......... .......... .......... 87% 48.8M 3s
232150K .......... .......... .......... .......... .......... 87% 35.6M 3s
232200K .......... .......... .......... .......... .......... 87% 16.0M 2s
232250K .......... .......... .......... .......... .......... 87% 20.5M 2s
232300K .......... .......... .......... .......... .......... 87% 34.1M 2s
232350K .......... .......... .......... .......... .......... 87% 15.0M 2s
232400K .......... .......... .......... .......... .......... 87% 15.8M 2s
232450K .......... .......... .......... .......... .......... 87% 31.1M 2s
232500K .......... .......... .......... .......... .......... 87% 13.7M 2s
232550K .......... .......... .......... .......... .......... 87% 27.2M 2s
232600K .......... .......... .......... .......... .......... 87% 24.5M 2s
232650K .......... .......... .......... .......... .......... 87% 21.0M 2s
232700K .......... .......... .......... .......... .......... 87% 16.7M 2s
232750K .......... .......... .......... .......... .......... 87% 35.8M 2s
232800K .......... .......... .......... .......... .......... 87% 15.8M 2s
232850K .......... .......... .......... .......... .......... 87% 17.5M 2s
232900K .......... .......... .......... .......... .......... 87% 35.2M 2s
232950K .......... .......... .......... .......... .......... 87% 16.5M 2s
233000K .......... .......... .......... .......... .......... 87% 19.3M 2s
233050K .......... .......... .......... .......... .......... 87% 24.5M 2s
233100K .......... .......... .......... .......... .......... 87% 19.7M 2s
233150K .......... .......... .......... .......... .......... 87% 16.0M 2s
233200K .......... .......... .......... .......... .......... 87% 21.0M 2s
233250K .......... .......... .......... .......... .......... 87% 23.3M 2s
233300K .......... .......... .......... .......... .......... 87% 22.9M 2s
233350K .......... .......... .......... .......... .......... 87% 17.5M 2s
233400K .......... .......... .......... .......... .......... 87% 16.8M 2s
233450K .......... .......... .......... .......... .......... 87% 16.5M 2s
233500K .......... .......... .......... .......... .......... 87% 22.8M 2s
233550K .......... .......... .......... .......... .......... 87% 152M 2s
233600K .......... .......... .......... .......... .......... 87% 13.2M 2s
233650K .......... .......... .......... .......... .......... 87% 18.9M 2s
233700K .......... .......... .......... .......... .......... 87% 13.6M 2s
233750K .......... .......... .......... .......... .......... 87% 23.5M 2s
233800K .......... .......... .......... .......... .......... 87% 25.8M 2s
233850K .......... .......... .......... .......... .......... 88% 21.8M 2s
233900K .......... .......... .......... .......... .......... 88% 18.7M 2s
233950K .......... .......... .......... .......... .......... 88% 14.4M 2s
234000K .......... .......... .......... .......... .......... 88% 25.1M 2s
234050K .......... .......... .......... .......... .......... 88% 15.0M 2s
234100K .......... .......... .......... .......... .......... 88% 17.4M 2s
234150K .......... .......... .......... .......... .......... 88% 29.4M 2s
234200K .......... .......... .......... .......... .......... 88% 13.1M 2s
234250K .......... .......... .......... .......... .......... 88% 16.1M 2s
234300K .......... .......... .......... .......... .......... 88% 29.8M 2s
234350K .......... .......... .......... .......... .......... 88% 17.9M 2s
234400K .......... .......... .......... .......... .......... 88% 14.9M 2s
234450K .......... .......... .......... .......... .......... 88% 33.7M 2s
234500K .......... .......... .......... .......... .......... 88% 26.6M 2s
234550K .......... .......... .......... .......... .......... 88% 10.7M 2s
234600K .......... .......... .......... .......... .......... 88% 20.2M 2s
234650K .......... .......... .......... .......... .......... 88% 31.8M 2s
234700K .......... .......... .......... .......... .......... 88% 10.6M 2s
234750K .......... .......... .......... .......... .......... 88% 42.4M 2s
234800K .......... .......... .......... .......... .......... 88% 35.0M 2s
234850K .......... .......... .......... .......... .......... 88% 12.3M 2s
234900K .......... .......... .......... .......... .......... 88% 17.1M 2s
234950K .......... .......... .......... .......... .......... 88% 29.6M 2s
235000K .......... .......... .......... .......... .......... 88% 27.7M 2s
235050K .......... .......... .......... .......... .......... 88% 9.64M 2s
235100K .......... .......... .......... .......... .......... 88% 20.9M 2s
235150K .......... .......... .......... .......... .......... 88% 23.7M 2s
235200K .......... .......... .......... .......... .......... 88% 11.9M 2s
235250K .......... .......... .......... .......... .......... 88% 21.7M 2s
235300K .......... .......... .......... .......... .......... 88% 36.8M 2s
235350K .......... .......... .......... .......... .......... 88% 14.3M 2s
235400K .......... .......... .......... .......... .......... 88% 11.9M 2s
235450K .......... .......... .......... .......... .......... 88% 32.0M 2s
235500K .......... .......... .......... .......... .......... 88% 19.9M 2s
235550K .......... .......... .......... .......... .......... 88% 10.8M 2s
235600K .......... .......... .......... .......... .......... 88% 24.6M 2s
235650K .......... .......... .......... .......... .......... 88% 14.5M 2s
235700K .......... .......... .......... .......... .......... 88% 16.5M 2s
235750K .......... .......... .......... .......... .......... 88% 9.10M 2s
235800K .......... .......... .......... .......... .......... 88% 38.3M 2s
235850K .......... .......... .......... .......... .......... 88% 12.0M 2s
235900K .......... .......... .......... .......... .......... 88% 7.89M 2s
235950K .......... .......... .......... .......... .......... 88% 25.6M 2s
236000K .......... .......... .......... .......... .......... 88% 22.3M 2s
236050K .......... .......... .......... .......... .......... 88% 9.76M 2s
236100K .......... .......... .......... .......... .......... 88% 13.1M 2s
236150K .......... .......... .......... .......... .......... 88% 37.2M 2s
236200K .......... .......... .......... .......... .......... 88% 10.2M 2s
236250K .......... .......... .......... .......... .......... 88% 11.4M 2s
236300K .......... .......... .......... .......... .......... 88% 20.5M 2s
236350K .......... .......... .......... .......... .......... 88% 14.7M 2s
236400K .......... .......... .......... .......... .......... 88% 13.5M 2s
236450K .......... .......... .......... .......... .......... 88% 12.0M 2s
236500K .......... .......... .......... .......... .......... 89% 38.3M 2s
236550K .......... .......... .......... .......... .......... 89% 10.4M 2s
236600K .......... .......... .......... .......... .......... 89% 8.64M 2s
236650K .......... .......... .......... .......... .......... 89% 30.5M 2s
236700K .......... .......... .......... .......... .......... 89% 10.1M 2s
236750K .......... .......... .......... .......... .......... 89% 14.1M 2s
236800K .......... .......... .......... .......... .......... 89% 13.5M 2s
236850K .......... .......... .......... .......... .......... 89% 17.0M 2s
236900K .......... .......... .......... .......... .......... 89% 12.7M 2s
236950K .......... .......... .......... .......... .......... 89% 11.3M 2s
237000K .......... .......... .......... .......... .......... 89% 46.5M 2s
237050K .......... .......... .......... .......... .......... 89% 14.3M 2s
237100K .......... .......... .......... .......... .......... 89% 19.5M 2s
237150K .......... .......... .......... .......... .......... 89% 17.8M 2s
237200K .......... .......... .......... .......... .......... 89% 22.1M 2s
237250K .......... .......... .......... .......... .......... 89% 18.2M 2s
237300K .......... .......... .......... .......... .......... 89% 11.8M 2s
237350K .......... .......... .......... .......... .......... 89% 25.9M 2s
237400K .......... .......... .......... .......... .......... 89% 21.7M 2s
237450K .......... .......... .......... .......... .......... 89% 15.6M 2s
237500K .......... .......... .......... .......... .......... 89% 17.6M 2s
237550K .......... .......... .......... .......... .......... 89% 20.1M 2s
237600K .......... .......... .......... .......... .......... 89% 18.9M 2s
237650K .......... .......... .......... .......... .......... 89% 11.5M 2s
237700K .......... .......... .......... .......... .......... 89% 39.3M 2s
237750K .......... .......... .......... .......... .......... 89% 17.9M 2s
237800K .......... .......... .......... .......... .......... 89% 17.2M 2s
237850K .......... .......... .......... .......... .......... 89% 13.6M 2s
237900K .......... .......... .......... .......... .......... 89% 29.3M 2s
237950K .......... .......... .......... .......... .......... 89% 16.8M 2s
238000K .......... .......... .......... .......... .......... 89% 12.6M 2s
238050K .......... .......... .......... .......... .......... 89% 28.7M 2s
238100K .......... .......... .......... .......... .......... 89% 17.1M 2s
238150K .......... .......... .......... .......... .......... 89% 29.7M 2s
238200K .......... .......... .......... .......... .......... 89% 14.4M 2s
238250K .......... .......... .......... .......... .......... 89% 33.1M 2s
238300K .......... .......... .......... .......... .......... 89% 25.0M 2s
238350K .......... .......... .......... .......... .......... 89% 14.3M 2s
238400K .......... .......... .......... .......... .......... 89% 27.6M 2s
238450K .......... .......... .......... .......... .......... 89% 16.6M 2s
238500K .......... .......... .......... .......... .......... 89% 18.3M 2s
238550K .......... .......... .......... .......... .......... 89% 32.1M 2s
238600K .......... .......... .......... .......... .......... 89% 22.7M 2s
238650K .......... .......... .......... .......... .......... 89% 33.0M 2s
238700K .......... .......... .......... .......... .......... 89% 9.68M 2s
238750K .......... .......... .......... .......... .......... 89% 34.3M 2s
238800K .......... .......... .......... .......... .......... 89% 27.4M 2s
238850K .......... .......... .......... .......... .......... 89% 28.3M 2s
238900K .......... .......... .......... .......... .......... 89% 15.0M 2s
238950K .......... .......... .......... .......... .......... 89% 28.0M 2s
239000K .......... .......... .......... .......... .......... 89% 25.6M 2s
239050K .......... .......... .......... .......... .......... 89% 37.7M 2s
239100K .......... .......... .......... .......... .......... 89% 12.7M 2s
239150K .......... .......... .......... .......... .......... 90% 16.2M 2s
239200K .......... .......... .......... .......... .......... 90% 37.5M 2s
239250K .......... .......... .......... .......... .......... 90% 18.4M 2s
239300K .......... .......... .......... .......... .......... 90% 30.8M 2s
239350K .......... .......... .......... .......... .......... 90% 18.3M 2s
239400K .......... .......... .......... .......... .......... 90% 41.3M 2s
239450K .......... .......... .......... .......... .......... 90% 13.9M 2s
239500K .......... .......... .......... .......... .......... 90% 43.3M 2s
239550K .......... .......... .......... .......... .......... 90% 16.1M 2s
239600K .......... .......... .......... .......... .......... 90% 42.4M 2s
239650K .......... .......... .......... .......... .......... 90% 14.4M 2s
239700K .......... .......... .......... .......... .......... 90% 30.2M 2s
239750K .......... .......... .......... .......... .......... 90% 19.4M 2s
239800K .......... .......... .......... .......... .......... 90% 50.4M 2s
239850K .......... .......... .......... .......... .......... 90% 14.2M 2s
239900K .......... .......... .......... .......... .......... 90% 16.3M 2s
239950K .......... .......... .......... .......... .......... 90% 53.7M 2s
240000K .......... .......... .......... .......... .......... 90% 43.0M 2s
240050K .......... .......... .......... .......... .......... 90% 12.8M 2s
240100K .......... .......... .......... .......... .......... 90% 19.5M 2s
240150K .......... .......... .......... .......... .......... 90% 26.1M 2s
240200K .......... .......... .......... .......... .......... 90% 36.4M 2s
240250K .......... .......... .......... .......... .......... 90% 14.1M 2s
240300K .......... .......... .......... .......... .......... 90% 15.4M 2s
240350K .......... .......... .......... .......... .......... 90% 42.3M 2s
240400K .......... .......... .......... .......... .......... 90% 20.9M 2s
240450K .......... .......... .......... .......... .......... 90% 22.4M 2s
240500K .......... .......... .......... .......... .......... 90% 17.5M 2s
240550K .......... .......... .......... .......... .......... 90% 40.0M 2s
240600K .......... .......... .......... .......... .......... 90% 15.8M 2s
240650K .......... .......... .......... .......... .......... 90% 37.6M 2s
240700K .......... .......... .......... .......... .......... 90% 15.5M 2s
240750K .......... .......... .......... .......... .......... 90% 24.7M 2s
240800K .......... .......... .......... .......... .......... 90% 24.4M 2s
240850K .......... .......... .......... .......... .......... 90% 14.6M 2s
240900K .......... .......... .......... .......... .......... 90% 43.9M 2s
240950K .......... .......... .......... .......... .......... 90% 42.2M 2s
241000K .......... .......... .......... .......... .......... 90% 12.9M 2s
241050K .......... .......... .......... .......... .......... 90% 18.9M 2s
241100K .......... .......... .......... .......... .......... 90% 22.9M 2s
241150K .......... .......... .......... .......... .......... 90% 39.7M 2s
241200K .......... .......... .......... .......... .......... 90% 17.1M 2s
241250K .......... .......... .......... .......... .......... 90% 14.2M 2s
241300K .......... .......... .......... .......... .......... 90% 25.7M 2s
241350K .......... .......... .......... .......... .......... 90% 38.5M 2s
241400K .......... .......... .......... .......... .......... 90% 20.5M 2s
241450K .......... .......... .......... .......... .......... 90% 13.1M 2s
241500K .......... .......... .......... .......... .......... 90% 36.3M 2s
241550K .......... .......... .......... .......... .......... 90% 45.7M 2s
241600K .......... .......... .......... .......... .......... 90% 20.0M 2s
241650K .......... .......... .......... .......... .......... 90% 14.1M 2s
241700K .......... .......... .......... .......... .......... 90% 34.6M 2s
241750K .......... .......... .......... .......... .......... 90% 21.7M 2s
241800K .......... .......... .......... .......... .......... 91% 19.6M 2s
241850K .......... .......... .......... .......... .......... 91% 17.3M 2s
241900K .......... .......... .......... .......... .......... 91% 29.1M 2s
241950K .......... .......... .......... .......... .......... 91% 17.5M 2s
242000K .......... .......... .......... .......... .......... 91% 17.5M 2s
242050K .......... .......... .......... .......... .......... 91% 30.3M 2s
242100K .......... .......... .......... .......... .......... 91% 36.1M 2s
242150K .......... .......... .......... .......... .......... 91% 14.9M 2s
242200K .......... .......... .......... .......... .......... 91% 21.2M 2s
242250K .......... .......... .......... .......... .......... 91% 18.7M 2s
242300K .......... .......... .......... .......... .......... 91% 57.8M 2s
242350K .......... .......... .......... .......... .......... 91% 12.4M 2s
242400K .......... .......... .......... .......... .......... 91% 54.7M 2s
242450K .......... .......... .......... .......... .......... 91% 21.3M 2s
242500K .......... .......... .......... .......... .......... 91% 16.6M 2s
242550K .......... .......... .......... .......... .......... 91% 37.8M 2s
242600K .......... .......... .......... .......... .......... 91% 15.1M 2s
242650K .......... .......... .......... .......... .......... 91% 27.0M 2s
242700K .......... .......... .......... .......... .......... 91% 19.8M 2s
242750K .......... .......... .......... .......... .......... 91% 23.6M 2s
242800K .......... .......... .......... .......... .......... 91% 19.8M 2s
242850K .......... .......... .......... .......... .......... 91% 22.5M 2s
242900K .......... .......... .......... .......... .......... 91% 18.3M 2s
242950K .......... .......... .......... .......... .......... 91% 21.5M 2s
243000K .......... .......... .......... .......... .......... 91% 17.9M 2s
243050K .......... .......... .......... .......... .......... 91% 29.9M 2s
243100K .......... .......... .......... .......... .......... 91% 15.2M 2s
243150K .......... .......... .......... .......... .......... 91% 34.2M 2s
243200K .......... .......... .......... .......... .......... 91% 17.3M 2s
243250K .......... .......... .......... .......... .......... 91% 38.0M 2s
243300K .......... .......... .......... .......... .......... 91% 15.8M 2s
243350K .......... .......... .......... .......... .......... 91% 14.5M 2s
243400K .......... .......... .......... .......... .......... 91% 24.8M 2s
243450K .......... .......... .......... .......... .......... 91% 12.8M 2s
243500K .......... .......... .......... .......... .......... 91% 104M 2s
243550K .......... .......... .......... .......... .......... 91% 16.3M 2s
243600K .......... .......... .......... .......... .......... 91% 4.20M 2s
243650K .......... .......... .......... .......... .......... 91% 15.0M 2s
243700K .......... .......... .......... .......... .......... 91% 31.8M 2s
243750K .......... .......... .......... .......... .......... 91% 111M 2s
243800K .......... .......... .......... .......... .......... 91% 14.8M 2s
243850K .......... .......... .......... .......... .......... 91% 36.0M 2s
243900K .......... .......... .......... .......... .......... 91% 75.8M 2s
243950K .......... .......... .......... .......... .......... 91% 122M 2s
244000K .......... .......... .......... .......... .......... 91% 23.0M 2s
244050K .......... .......... .......... .......... .......... 91% 38.2M 2s
244100K .......... .......... .......... .......... .......... 91% 17.7M 2s
244150K .......... .......... .......... .......... .......... 91% 13.6M 2s
244200K .......... .......... .......... .......... .......... 91% 22.9M 2s
244250K .......... .......... .......... .......... .......... 91% 26.8M 2s
244300K .......... .......... .......... .......... .......... 91% 13.9M 2s
244350K .......... .......... .......... .......... .......... 91% 22.3M 2s
244400K .......... .......... .......... .......... .......... 91% 14.8M 2s
244450K .......... .......... .......... .......... .......... 92% 24.2M 2s
244500K .......... .......... .......... .......... .......... 92% 14.7M 2s
244550K .......... .......... .......... .......... .......... 92% 13.8M 2s
244600K .......... .......... .......... .......... .......... 92% 25.7M 2s
244650K .......... .......... .......... .......... .......... 92% 20.9M 2s
244700K .......... .......... .......... .......... .......... 92% 11.0M 2s
244750K .......... .......... .......... .......... .......... 92% 16.2M 2s
244800K .......... .......... .......... .......... .......... 92% 20.1M 2s
244850K .......... .......... .......... .......... .......... 92% 20.9M 2s
244900K .......... .......... .......... .......... .......... 92% 17.8M 2s
244950K .......... .......... .......... .......... .......... 92% 12.3M 2s
245000K .......... .......... .......... .......... .......... 92% 51.5M 2s
245050K .......... .......... .......... .......... .......... 92% 4.50M 2s
245100K .......... .......... .......... .......... .......... 92% 74.4M 2s
245150K .......... .......... .......... .......... .......... 92% 70.6M 2s
245200K .......... .......... .......... .......... .......... 92% 43.7M 2s
245250K .......... .......... .......... .......... .......... 92% 101M 1s
245300K .......... .......... .......... .......... .......... 92% 30.3M 1s
245350K .......... .......... .......... .......... .......... 92% 9.77M 1s
245400K .......... .......... .......... .......... .......... 92% 60.0M 1s
245450K .......... .......... .......... .......... .......... 92% 9.25M 1s
245500K .......... .......... .......... .......... .......... 92% 58.2M 1s
245550K .......... .......... .......... .......... .......... 92% 11.2M 1s
245600K .......... .......... .......... .......... .......... 92% 19.6M 1s
245650K .......... .......... .......... .......... .......... 92% 10.8M 1s
245700K .......... .......... .......... .......... .......... 92% 41.4M 1s
245750K .......... .......... .......... .......... .......... 92% 11.4M 1s
245800K .......... .......... .......... .......... .......... 92% 24.2M 1s
245850K .......... .......... .......... .......... .......... 92% 11.3M 1s
245900K .......... .......... .......... .......... .......... 92% 30.4M 1s
245950K .......... .......... .......... .......... .......... 92% 9.91M 1s
246000K .......... .......... .......... .......... .......... 92% 28.7M 1s
246050K .......... .......... .......... .......... .......... 92% 11.0M 1s
246100K .......... .......... .......... .......... .......... 92% 20.7M 1s
246150K .......... .......... .......... .......... .......... 92% 12.3M 1s
246200K .......... .......... .......... .......... .......... 92% 29.4M 1s
246250K .......... .......... .......... .......... .......... 92% 12.5M 1s
246300K .......... .......... .......... .......... .......... 92% 7.25M 1s
246350K .......... .......... .......... .......... .......... 92% 26.8M 1s
246400K .......... .......... .......... .......... .......... 92% 54.3M 1s
246450K .......... .......... .......... .......... .......... 92% 37.7M 1s
246500K .......... .......... .......... .......... .......... 92% 13.0M 1s
246550K .......... .......... .......... .......... .......... 92% 29.1M 1s
246600K .......... .......... .......... .......... .......... 92% 12.8M 1s
246650K .......... .......... .......... .......... .......... 92% 11.7M 1s
246700K .......... .......... .......... .......... .......... 92% 11.5M 1s
246750K .......... .......... .......... .......... .......... 92% 21.6M 1s
246800K .......... .......... .......... .......... .......... 92% 19.1M 1s
246850K .......... .......... .......... .......... .......... 92% 11.9M 1s
246900K .......... .......... .......... .......... .......... 92% 12.4M 1s
246950K .......... .......... .......... .......... .......... 92% 24.5M 1s
247000K .......... .......... .......... .......... .......... 92% 14.8M 1s
247050K .......... .......... .......... .......... .......... 92% 11.5M 1s
247100K .......... .......... .......... .......... .......... 93% 11.0M 1s
247150K .......... .......... .......... .......... .......... 93% 20.5M 1s
247200K .......... .......... .......... .......... .......... 93% 16.4M 1s
247250K .......... .......... .......... .......... .......... 93% 30.3M 1s
247300K .......... .......... .......... .......... .......... 93% 11.3M 1s
247350K .......... .......... .......... .......... .......... 93% 15.3M 1s
247400K .......... .......... .......... .......... .......... 93% 14.5M 1s
247450K .......... .......... .......... .......... .......... 93% 17.4M 1s
247500K .......... .......... .......... .......... .......... 93% 12.8M 1s
247550K .......... .......... .......... .......... .......... 93% 17.8M 1s
247600K .......... .......... .......... .......... .......... 93% 19.2M 1s
247650K .......... .......... .......... .......... .......... 93% 15.2M 1s
247700K .......... .......... .......... .......... .......... 93% 14.8M 1s
247750K .......... .......... .......... .......... .......... 93% 18.2M 1s
247800K .......... .......... .......... .......... .......... 93% 19.5M 1s
247850K .......... .......... .......... .......... .......... 93% 17.0M 1s
247900K .......... .......... .......... .......... .......... 93% 10.8M 1s
247950K .......... .......... .......... .......... .......... 93% 19.8M 1s
248000K .......... .......... .......... .......... .......... 93% 15.7M 1s
248050K .......... .......... .......... .......... .......... 93% 16.3M 1s
248100K .......... .......... .......... .......... .......... 93% 14.7M 1s
248150K .......... .......... .......... .......... .......... 93% 6.25M 1s
248200K .......... .......... .......... .......... .......... 93% 65.4M 1s
248250K .......... .......... .......... .......... .......... 93% 34.5M 1s
248300K .......... .......... .......... .......... .......... 93% 13.6M 1s
248350K .......... .......... .......... .......... .......... 93% 7.70M 1s
248400K .......... .......... .......... .......... .......... 93% 39.7M 1s
248450K .......... .......... .......... .......... .......... 93% 8.81M 1s
248500K .......... .......... .......... .......... .......... 93% 13.3M 1s
248550K .......... .......... .......... .......... .......... 93% 11.4M 1s
248600K .......... .......... .......... .......... .......... 93% 11.4M 1s
248650K .......... .......... .......... .......... .......... 93% 11.8M 1s
248700K .......... .......... .......... .......... .......... 93% 10.6M 1s
248750K .......... .......... .......... .......... .......... 93% 17.0M 1s
248800K .......... .......... .......... .......... .......... 93% 18.7M 1s
248850K .......... .......... .......... .......... .......... 93% 10.0M 1s
248900K .......... .......... .......... .......... .......... 93% 9.98M 1s
248950K .......... .......... .......... .......... .......... 93% 11.4M 1s
249000K .......... .......... .......... .......... .......... 93% 11.1M 1s
249050K .......... .......... .......... .......... .......... 93% 33.1M 1s
249100K .......... .......... .......... .......... .......... 93% 9.82M 1s
249150K .......... .......... .......... .......... .......... 93% 9.84M 1s
249200K .......... .......... .......... .......... .......... 93% 10.2M 1s
249250K .......... .......... .......... .......... .......... 93% 25.3M 1s
249300K .......... .......... .......... .......... .......... 93% 14.8M 1s
249350K .......... .......... .......... .......... .......... 93% 9.42M 1s
249400K .......... .......... .......... .......... .......... 93% 10.1M 1s
249450K .......... .......... .......... .......... .......... 93% 19.0M 1s
249500K .......... .......... .......... .......... .......... 93% 14.2M 1s
249550K .......... .......... .......... .......... .......... 93% 10.8M 1s
249600K .......... .......... .......... .......... .......... 93% 9.02M 1s
249650K .......... .......... .......... .......... .......... 93% 11.9M 1s
249700K .......... .......... .......... .......... .......... 93% 10.8M 1s
249750K .......... .......... .......... .......... .......... 94% 16.6M 1s
249800K .......... .......... .......... .......... .......... 94% 13.9M 1s
249850K .......... .......... .......... .......... .......... 94% 10.3M 1s
249900K .......... .......... .......... .......... .......... 94% 9.13M 1s
249950K .......... .......... .......... .......... .......... 94% 17.3M 1s
250000K .......... .......... .......... .......... .......... 94% 13.3M 1s
250050K .......... .......... .......... .......... .......... 94% 9.61M 1s
250100K .......... .......... .......... .......... .......... 94% 10.2M 1s
250150K .......... .......... .......... .......... .......... 94% 22.6M 1s
250200K .......... .......... .......... .......... .......... 94% 12.0M 1s
250250K .......... .......... .......... .......... .......... 94% 9.41M 1s
250300K .......... .......... .......... .......... .......... 94% 21.1M 1s
250350K .......... .......... .......... .......... .......... 94% 14.2M 1s
250400K .......... .......... .......... .......... .......... 94% 8.99M 1s
250450K .......... .......... .......... .......... .......... 94% 13.2M 1s
250500K .......... .......... .......... .......... .......... 94% 14.8M 1s
250550K .......... .......... .......... .......... .......... 94% 10.7M 1s
250600K .......... .......... .......... .......... .......... 94% 23.5M 1s
250650K .......... .......... .......... .......... .......... 94% 12.1M 1s
250700K .......... .......... .......... .......... .......... 94% 9.22M 1s
250750K .......... .......... .......... .......... .......... 94% 18.2M 1s
250800K .......... .......... .......... .......... .......... 94% 14.1M 1s
250850K .......... .......... .......... .......... .......... 94% 6.01M 1s
250900K .......... .......... .......... .......... .......... 94% 133M 1s
250950K .......... .......... .......... .......... .......... 94% 10.3M 1s
251000K .......... .......... .......... .......... .......... 94% 12.3M 1s
251050K .......... .......... .......... .......... .......... 94% 10.8M 1s
251100K .......... .......... .......... .......... .......... 94% 10.3M 1s
251150K .......... .......... .......... .......... .......... 94% 9.64M 1s
251200K .......... .......... .......... .......... .......... 94% 10.9M 1s
251250K .......... .......... .......... .......... .......... 94% 9.64M 1s
251300K .......... .......... .......... .......... .......... 94% 11.7M 1s
251350K .......... .......... .......... .......... .......... 94% 14.7M 1s
251400K .......... .......... .......... .......... .......... 94% 8.88M 1s
251450K .......... .......... .......... .......... .......... 94% 9.85M 1s
251500K .......... .......... .......... .......... .......... 94% 15.0M 1s
251550K .......... .......... .......... .......... .......... 94% 10.2M 1s
251600K .......... .......... .......... .......... .......... 94% 8.97M 1s
251650K .......... .......... .......... .......... .......... 94% 9.81M 1s
251700K .......... .......... .......... .......... .......... 94% 11.4M 1s
251750K .......... .......... .......... .......... .......... 94% 10.0M 1s
251800K .......... .......... .......... .......... .......... 94% 16.2M 1s
251850K .......... .......... .......... .......... .......... 94% 9.81M 1s
251900K .......... .......... .......... .......... .......... 94% 11.5M 1s
251950K .......... .......... .......... .......... .......... 94% 10.3M 1s
252000K .......... .......... .......... .......... .......... 94% 16.8M 1s
252050K .......... .......... .......... .......... .......... 94% 9.84M 1s
252100K .......... .......... .......... .......... .......... 94% 9.29M 1s
252150K .......... .......... .......... .......... .......... 94% 32.2M 1s
252200K .......... .......... .......... .......... .......... 94% 9.15M 1s
252250K .......... .......... .......... .......... .......... 94% 13.4M 1s
252300K .......... .......... .......... .......... .......... 94% 11.9M 1s
252350K .......... .......... .......... .......... .......... 94% 7.65M 1s
252400K .......... .......... .......... .......... .......... 94% 25.5M 1s
252450K .......... .......... .......... .......... .......... 95% 10.4M 1s
252500K .......... .......... .......... .......... .......... 95% 10.8M 1s
252550K .......... .......... .......... .......... .......... 95% 11.0M 1s
252600K .......... .......... .......... .......... .......... 95% 7.64M 1s
252650K .......... .......... .......... .......... .......... 95% 21.6M 1s
252700K .......... .......... .......... .......... .......... 95% 7.45M 1s
252750K .......... .......... .......... .......... .......... 95% 11.7M 1s
252800K .......... .......... .......... .......... .......... 95% 24.7M 1s
252850K .......... .......... .......... .......... .......... 95% 10.7M 1s
252900K .......... .......... .......... .......... .......... 95% 12.0M 1s
252950K .......... .......... .......... .......... .......... 95% 12.0M 1s
253000K .......... .......... .......... .......... .......... 95% 10.4M 1s
253050K .......... .......... .......... .......... .......... 95% 14.3M 1s
253100K .......... .......... .......... .......... .......... 95% 10.5M 1s
253150K .......... .......... .......... .......... .......... 95% 13.3M 1s
253200K .......... .......... .......... .......... .......... 95% 11.7M 1s
253250K .......... .......... .......... .......... .......... 95% 87.2M 1s
253300K .......... .......... .......... .......... .......... 95% 11.1M 1s
253350K .......... .......... .......... .......... .......... 95% 10.3M 1s
253400K .......... .......... .......... .......... .......... 95% 11.3M 1s
253450K .......... .......... .......... .......... .......... 95% 10.2M 1s
253500K .......... .......... .......... .......... .......... 95% 11.0M 1s
253550K .......... .......... .......... .......... .......... 95% 60.4M 1s
253600K .......... .......... .......... .......... .......... 95% 11.7M 1s
253650K .......... .......... .......... .......... .......... 95% 8.88M 1s
253700K .......... .......... .......... .......... .......... 95% 9.43M 1s
253750K .......... .......... .......... .......... .......... 95% 93.3M 1s
253800K .......... .......... .......... .......... .......... 95% 10.5M 1s
253850K .......... .......... .......... .......... .......... 95% 10.2M 1s
253900K .......... .......... .......... .......... .......... 95% 12.7M 1s
253950K .......... .......... .......... .......... .......... 95% 10.3M 1s
254000K .......... .......... .......... .......... .......... 95% 67.1M 1s
254050K .......... .......... .......... .......... .......... 95% 9.83M 1s
254100K .......... .......... .......... .......... .......... 95% 11.5M 1s
254150K .......... .......... .......... .......... .......... 95% 10.9M 1s
254200K .......... .......... .......... .......... .......... 95% 43.2M 1s
254250K .......... .......... .......... .......... .......... 95% 10.9M 1s
254300K .......... .......... .......... .......... .......... 95% 9.84M 1s
254350K .......... .......... .......... .......... .......... 95% 9.24M 1s
254400K .......... .......... .......... .......... .......... 95% 45.8M 1s
254450K .......... .......... .......... .......... .......... 95% 8.70M 1s
254500K .......... .......... .......... .......... .......... 95% 12.1M 1s
254550K .......... .......... .......... .......... .......... 95% 31.3M 1s
254600K .......... .......... .......... .......... .......... 95% 9.82M 1s
254650K .......... .......... .......... .......... .......... 95% 10.9M 1s
254700K .......... .......... .......... .......... .......... 95% 29.6M 1s
254750K .......... .......... .......... .......... .......... 95% 8.51M 1s
254800K .......... .......... .......... .......... .......... 95% 10.8M 1s
254850K .......... .......... .......... .......... .......... 95% 34.7M 1s
254900K .......... .......... .......... .......... .......... 95% 10.0M 1s
254950K .......... .......... .......... .......... .......... 95% 8.78M 1s
255000K .......... .......... .......... .......... .......... 95% 34.2M 1s
255050K .......... .......... .......... .......... .......... 95% 12.5M 1s
255100K .......... .......... .......... .......... .......... 96% 9.42M 1s
255150K .......... .......... .......... .......... .......... 96% 42.6M 1s
255200K .......... .......... .......... .......... .......... 96% 9.79M 1s
255250K .......... .......... .......... .......... .......... 96% 26.2M 1s
255300K .......... .......... .......... .......... .......... 96% 9.49M 1s
255350K .......... .......... .......... .......... .......... 96% 9.72M 1s
255400K .......... .......... .......... .......... .......... 96% 38.9M 1s
255450K .......... .......... .......... .......... .......... 96% 8.96M 1s
255500K .......... .......... .......... .......... .......... 96% 10.6M 1s
255550K .......... .......... .......... .......... .......... 96% 29.5M 1s
255600K .......... .......... .......... .......... .......... 96% 9.87M 1s
255650K .......... .......... .......... .......... .......... 96% 50.8M 1s
255700K .......... .......... .......... .......... .......... 96% 8.43M 1s
255750K .......... .......... .......... .......... .......... 96% 11.0M 1s
255800K .......... .......... .......... .......... .......... 96% 35.3M 1s
255850K .......... .......... .......... .......... .......... 96% 8.56M 1s
255900K .......... .......... .......... .......... .......... 96% 12.5M 1s
255950K .......... .......... .......... .......... .......... 96% 20.9M 1s
256000K .......... .......... .......... .......... .......... 96% 8.75M 1s
256050K .......... .......... .......... .......... .......... 96% 43.7M 1s
256100K .......... .......... .......... .......... .......... 96% 9.87M 1s
256150K .......... .......... .......... .......... .......... 96% 59.0M 1s
256200K .......... .......... .......... .......... .......... 96% 7.77M 1s
256250K .......... .......... .......... .......... .......... 96% 9.98M 1s
256300K .......... .......... .......... .......... .......... 96% 53.0M 1s
256350K .......... .......... .......... .......... .......... 96% 8.74M 1s
256400K .......... .......... .......... .......... .......... 96% 39.2M 1s
256450K .......... .......... .......... .......... .......... 96% 8.82M 1s
256500K .......... .......... .......... .......... .......... 96% 38.0M 1s
256550K .......... .......... .......... .......... .......... 96% 8.97M 1s
256600K .......... .......... .......... .......... .......... 96% 35.2M 1s
256650K .......... .......... .......... .......... .......... 96% 8.77M 1s
256700K .......... .......... .......... .......... .......... 96% 17.0M 1s
256750K .......... .......... .......... .......... .......... 96% 15.5M 1s
256800K .......... .......... .......... .......... .......... 96% 19.3M 1s
256850K .......... .......... .......... .......... .......... 96% 17.2M 1s
256900K .......... .......... .......... .......... .......... 96% 11.2M 1s
256950K .......... .......... .......... .......... .......... 96% 33.6M 1s
257000K .......... .......... .......... .......... .......... 96% 10.7M 1s
257050K .......... .......... .......... .......... .......... 96% 38.0M 1s
257100K .......... .......... .......... .......... .......... 96% 9.20M 1s
257150K .......... .......... .......... .......... .......... 96% 15.1M 1s
257200K .......... .......... .......... .......... .......... 96% 18.7M 1s
257250K .......... .......... .......... .......... .......... 96% 16.6M 1s
257300K .......... .......... .......... .......... .......... 96% 21.0M 1s
257350K .......... .......... .......... .......... .......... 96% 5.46M 1s
257400K .......... .......... .......... .......... .......... 96% 15.6M 1s
257450K .......... .......... .......... .......... .......... 96% 68.8M 1s
257500K .......... .......... .......... .......... .......... 96% 17.6M 1s
257550K .......... .......... .......... .......... .......... 96% 17.8M 1s
257600K .......... .......... .......... .......... .......... 96% 14.8M 1s
257650K .......... .......... .......... .......... .......... 96% 12.7M 1s
257700K .......... .......... .......... .......... .......... 96% 20.1M 1s
257750K .......... .......... .......... .......... .......... 97% 12.4M 1s
257800K .......... .......... .......... .......... .......... 97% 12.7M 1s
257850K .......... .......... .......... .......... .......... 97% 11.0M 1s
257900K .......... .......... .......... .......... .......... 97% 13.4M 1s
257950K .......... .......... .......... .......... .......... 97% 18.1M 1s
258000K .......... .......... .......... .......... .......... 97% 12.4M 1s
258050K .......... .......... .......... .......... .......... 97% 12.7M 1s
258100K .......... .......... .......... .......... .......... 97% 13.2M 1s
258150K .......... .......... .......... .......... .......... 97% 21.8M 1s
258200K .......... .......... .......... .......... .......... 97% 9.18M 1s
258250K .......... .......... .......... .......... .......... 97% 12.2M 1s
258300K .......... .......... .......... .......... .......... 97% 14.7M 1s
258350K .......... .......... .......... .......... .......... 97% 21.0M 1s
258400K .......... .......... .......... .......... .......... 97% 11.1M 1s
258450K .......... .......... .......... .......... .......... 97% 12.7M 1s
258500K .......... .......... .......... .......... .......... 97% 12.3M 1s
258550K .......... .......... .......... .......... .......... 97% 20.6M 1s
258600K .......... .......... .......... .......... .......... 97% 4.29M 1s
258650K .......... .......... .......... .......... .......... 97% 36.9M 1s
258700K .......... .......... .......... .......... .......... 97% 95.2M 1s
258750K .......... .......... .......... .......... .......... 97% 13.6M 1s
258800K .......... .......... .......... .......... .......... 97% 12.6M 1s
258850K .......... .......... .......... .......... .......... 97% 14.0M 1s
258900K .......... .......... .......... .......... .......... 97% 19.9M 0s
258950K .......... .......... .......... .......... .......... 97% 12.6M 0s
259000K .......... .......... .......... .......... .......... 97% 12.1M 0s
259050K .......... .......... .......... .......... .......... 97% 12.8M 0s
259100K .......... .......... .......... .......... .......... 97% 12.7M 0s
259150K .......... .......... .......... .......... .......... 97% 13.6M 0s
259200K .......... .......... .......... .......... .......... 97% 12.2M 0s
259250K .......... .......... .......... .......... .......... 97% 11.2M 0s
259300K .......... .......... .......... .......... .......... 97% 13.4M 0s
259350K .......... .......... .......... .......... .......... 97% 14.6M 0s
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2024-05-30 12:19:09 (13.4 MB/s) - ‘ESPbeta.tgz’ saved [272121672/272121672]
+ 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/7.8/LINUX64/EngSketchPad/config/
+ ./makeEnv
ESP runtime AutoConfigurator
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0 with contents:
bin
include
lib
share
Info: Python exec /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad
EFCOMP = gfortran
CARCH = LINUX64
CASROOT = /home/jenkins/util/ESP/OpenCASCADE-7.8.0
CASARCH = .
CASREV = 7.8
PYTHONINC= /home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11
PYTHONLIB= -L/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib -lpython3.11
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESPenv.sh
++ export ESP_ARCH=LINUX64
++ ESP_ARCH=LINUX64
++ export ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ ESP_ROOT=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad
++ export CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ CASROOT=/home/jenkins/util/ESP/OpenCASCADE-7.8.0
++ export CASARCH=.
++ CASARCH=.
++ export CASREV=7.8
++ CASREV=7.8
++ export PATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP_venv/bin:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/test:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EGADS/trunk/pyEGADS::/home/jenkins/util/SU2/SU2-v8.0.0/bin
++ PYTHONPATH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/CAPS/pyCAPS:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/OpenCSM/trunk/pyOCSM:/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib: ']'
++ export LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ LD_LIBRARY_PATH=/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib:/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/ESP/LINUX64/lib:/home/jenkins/util/ESP/OpenCASCADE-7.8.0/lib:/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/lib:
++ export CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise/glyph
++ CAPS_GLYPH=/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ SLUGS_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/SLUGS/Slugs.html &'
++ export 'ESP_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ ESP_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/ESP/ESP.html &'
++ export 'WV_START=firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
++ WV_START='firefox /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/wvClient/wv.html &'
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src
+ make
(cd EGADS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
cp -p ../include/LINUX64 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/LINUX64
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
cp -p ../include/STANALYZER.make /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/STANALYZER.make
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
cp -p ../include/egads.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
cp -p ../include/egads_dot.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads_dot.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
cp -p ../include/egads.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egads.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
cp -p ../include/egadsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
cp -p ../include/egadsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
cp -p ../include/emp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/emp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
cp -p ../include/prm.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/prm.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
cp -p ../include/wsserver.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
cp -p ../include/wsserver.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsserver.inc
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
cp -p ../include/wsss.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/wsss.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
cp -p egadsTris.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsTris.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
cp -p egadsSplineFit.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineFit.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
cp -p egadsSplineVels.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsSplineVels.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
cp -p ../include/egadsf90.inc /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egadsf90.inc
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealD_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealD_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Lazy.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Lazy.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/SurrealS_Trad.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal/SurrealS_Trad.h
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/Surreal
cp Surreal/always_inline.h /home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsGeom.cpp -o ./egadsGeom.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsHLevel.cpp -o ./egadsHLevel.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTopo.cpp -o ./egadsTopo.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsCopy.cpp -o ./egadsCopy.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSpline.cpp -o ./egadsSpline.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsIO.cpp -o ./egadsIO.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSplineFit.cpp -o ./egadsSplineFit.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsSkinning.cpp -o ./egadsSkinning.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include \
-I. egadsTessSens.cpp -o ./egadsTessSens.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 OCC/BRepLib_FuseEdges.cpp -o ./BRepLib_FuseEdges.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsBase.c -o ./egadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsMemory.c -o ./egadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsAttrs.c -o ./egadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTess.c -o ./egadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTessInp.c -o ./egadsTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsTris.c -o ./egadsTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsQuads.c -o ./egadsQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsFit.c -o ./egadsFit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsRobust.c -o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSBO.c -o ./egadsSBO.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmCfit.c -o ./prmCfit.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmGrid.c -o ./prmGrid.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap prmUV.c -o ./prmUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsExport.c -o ./egadsExport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsEffect.c -o ./egadsEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I../util \
-I../util/uvmap egadsSolids.c -o ./egadsSolids.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include ../util/emp.c \
-o ./emp.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -IOCC -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/evaluate.c -o ./evaluate.o
g++ -g -x c++ -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I. -I../include \
../util/rational.c -o ./rational.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/inc -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0/include/opencascade -I/home/jenkins/util/ESP/OpenCASCADE-7.8.0 -I../include -I../util \
../util/regQuads.c -o ./regQuads.o
g++ -g -o ./SurrealD1 -O -std=c++11 -I. ../util/SurrealD1_btest.cpp
./SurrealD1
SurrealD1_test_suite Complete!
g++ -g -o ./SurrealD4 -O -std=c++11 -I. ../util/SurrealD4_btest.cpp
./SurrealD4
SurrealD4_test_suite Complete!
g++ -g -o ./SurrealS1 -O -std=c++11 -I. ../util/SurrealS1_btest.cpp
./SurrealS1
SurrealS1_test_suite Complete!
g++ -g -o ./SurrealS4 -O -std=c++11 -I. ../util/SurrealS4_btest.cpp
../util/SurrealS4_btest.cpp: In function ‘void multiply_deriv2()’:
../util/SurrealS4_btest.cpp:1265:23: note: variable tracking size limit exceeded with -fvar-tracking-assignments, retrying without
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/7.8/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=7.8 uvmap/main/uvmap.c -Iuvmap \
-o ./uvmap.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_bnd_adj.c -o ./uvmap_bnd_adj.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfibf.c -o ./uvmap_ibfibf.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_message.c -o ./uvmap_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibfin.c -o ./uvmap_ibfin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_read.c -o ./uvmap_read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccin.c -o ./uvmap_iccin.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_add.c -o ./uvmap_add.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_cpu_message.c -o ./uvmap_cpu_message.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapFindUV.c -o ./EG_uvmapFindUV.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapTest.c -o ./EG_uvmapTest.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inibe.c -o ./uvmap_inibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_version.c -o ./uvmap_version.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_inl_uv_bnd.c -o ./uvmap_inl_uv_bnd.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_edge_ratio.c -o ./uvmap_chk_edge_ratio.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_struct_tasks.c -o ./uvmap_struct_tasks.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Read.c -o ./EG_uvmap_Read.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_idibe.c -o ./uvmap_idibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapStructFree.c -o ./EG_uvmapStructFree.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmapGen.c -o ./EG_uvmapGen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_write.c -o ./uvmap_write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_ibeibe.c -o ./uvmap_ibeibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_chk_area_uv.c -o ./uvmap_chk_area_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_norm_uv.c -o ./uvmap_norm_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_iccibe.c -o ./uvmap_iccibe.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_malloc.c -o ./uvmap_malloc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen_uv.c -o ./uvmap_gen_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_to_egads.c -o ./uvmap_to_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/EG_uvmap_Write.c -o ./EG_uvmap_Write.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_test.c -o ./uvmap_test.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_mben_disc.c -o ./uvmap_mben_disc.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_find_uv.c -o ./uvmap_find_uv.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_gen.c -o ./uvmap_gen.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_solve.c -o ./uvmap_solve.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I. uvmap/uvmap_from_egads.c -o ./uvmap_from_egads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 egadsUVmap.c -Iuvmap \
-o ./egadsUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/libuvmap.a
gcc -g -o ./uvmap.exe ./uvmap.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/util'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegads.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -luvmap -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm -lstdc++ -lrt )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libuvmap.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadstatic.a
(cd .; \
ar rs /home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include fgadsBase.c -o ./fgadsBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsMemory.c -o ./fgadsMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsAttrs.c -o ./fgadsAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTess.c -o ./fgadsTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsHLevel.c -o ./fgadsHLevel.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsGeom.c -o ./fgadsGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include fgadsTopo.c -o ./fgadsTopo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libfgads.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/libfgads.a
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a emp.o; )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libemp.a
*** EGADS Build Complete! ***
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/src'
(cd EGADS/lite; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I. -I../src -I../util/uvmap \
liteBase.c -o ./liteBase.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteMemory.c -o ./liteMemory.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteGeom.c -o ./liteGeom.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteTopo.c -o ./liteTopo.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteAttrs.c -o ./liteAttrs.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteImport.c -o ./liteImport.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src -I../util/uvmap \
liteString.c -o ./liteString.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTess.c -o ./liteTess.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsTris.c -o ./liteTris.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -I../include -I. -I../src \
../src/egadsQuads.c -o ./liteQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util ../src/egadsTessInp.c -o ./liteTessInp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 ../src/egadsRobust.c \
-o ./egadsRobust.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLINUX64 -I../include ../util/emp.c \
-o ./emp.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../util/evaluate.c -o ./evaLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE ../util/rational.c \
-o ./ratLite.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I../util \
../util/regQuads.c -o ./liteRegQuads.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
../src/egadsEffect.c -o ./liteEffect.o
gcc -g -c -O -fno-unit-at-a-time -fPIC -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -DREVISION=7.8 -DLITE -I../include -I. -I../src \
-I../util/uvmap liteUVmap.c -o ./liteUVmap.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslite.so
(cd .; gcc -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/libegadslitestatic.a
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/lite'
(cd wvServer; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/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/7.8/LINUX64/EngSketchPad/include fwv.c -o ./fwv.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a
(cd .; ar rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/LINUX64/EngSketchPad/include -I. -o ./servertest.o
g++ -g -o ./server ./servertest.o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.a \
-lpthread -lz -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libwsserver.so
(cd .; g++ -g -shared -Wl,-no-undefined \
-o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/wvServer'
(cd EGADS/examples; make -f egads2cart.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include egads2cart.c \
-o ./egads2cart.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cart ./egads2cart.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
-lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vCurvature.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vCurvature.c -o ./vCurvature.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vCurvature ./vCurvature.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vGeom.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vGeom.c -o ./vGeom.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vGeom ./vGeom.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads \
-lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd EGADS/examples; make -f vTess.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ../util/retessFaces.c \
-o ./retessFaces.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTesstatic ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legadstatic -L/home/jenkins/util/ESP/OpenCASCADE-7.8.0/./lib -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lTKBool -lTKernel -lTKFeat -lTKBO -lTKGeomAlgo -lTKMath -lTKOffset -lTKPrim -lTKTopAlgo -lTKBRep -lTKG2d -lTKG3d -lTKGeomBase -lTKShHealing -lTKDESTEP -lTKDEIGES -lTKXSBase -lTKFillet -pthread -lm \
-lpthread -lz -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/vTess ./vTess.o ./retessFaces.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lwsserver -legads -lrt
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/EGADS/examples'
(cd OpenCSM; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. tim.c -o ./tim.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libocsm.so ./OpenCSM.o ./udp.o ./tim.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lwsserver -ldl -lrt -lm
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveCSM ./serveCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. serveESP.c -o ./serveESP.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/serveESP ./serveESP.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. sensCSM.c -o ./sensCSM.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/sensCSM ./sensCSM.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBezier.c -o ./udpBezier.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bezier.so ./udpBezier.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBiconvex.c -o ./udpBiconvex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/biconvex.so ./udpBiconvex.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBox.c -o ./udpBox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/box.so ./udpBox.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpBspline.c -o ./udpBspline.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bspline.so ./udpBspline.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCatmull.c -o ./udfCatmull.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/catmull.so ./udfCatmull.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCompare.c -o ./udfCompare.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/compare.so ./udfCompare.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreateBEM.c -o ./udfCreateBEM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createBEM.so ./udfCreateBEM.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfCreatePoly.c -o ./udfCreatePoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/createPoly.so ./udfCreatePoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpCsm.c -o ./udpCsm.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/csm.so ./udpCsm.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDeform.c -o ./udfDeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/deform.so ./udfDeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDroop.c -o ./udfDroop.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/droop.so ./udfDroop.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfDumpPmtrs.c -o ./udfDumpPmtrs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/dumpPmtrs.so ./udfDumpPmtrs.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfEditAttr.c -o ./udfEditAttr.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/editAttr.so ./udfEditAttr.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEllipse.c -o ./udpEllipse.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ellipse.so ./udpEllipse.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpEqn2body.c -o ./udpEqn2body.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/eqn2body.so ./udpEqn2body.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFitcurve.c -o ./udpFitcurve.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fitcurve.so ./udpFitcurve.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfFlend.c -o ./udfFlend.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flend.so ./udfFlend.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpFreeform.c -o ./udpFreeform.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/freeform.so ./udpFreeform.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGanged.c -o ./udfGanged.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ganged.so ./udfGanged.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfGuide.c -o ./udfGuide.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/guide.so ./udfGuide.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpHex.c -o ./udpHex.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hex.so ./udpHex.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpImport.c -o ./udpImport.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/import.so ./udpImport.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpKulfan.c -o ./udpKulfan.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/kulfan.so ./udpKulfan.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfLinalg.c -o ./udfLinalg.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/linalg.so ./udfLinalg.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMatchBodys.c -o ./udfMatchBodys.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/matchBodys.so ./udfMatchBodys.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfMechanism.c -o ./udfMechanism.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mechanism.so ./udfMechanism.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNaca.c -o ./udpNaca.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca.so ./udpNaca.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNaca6mc.c -o ./udfNaca6mc.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca6mc.so ./udfNaca6mc.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNacelle.c -o ./udfNacelle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nacelle.so ./udfNacelle.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpNurbbody.c -o ./udpNurbbody.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nurbbody.so ./udpNurbbody.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfNuscale.c -o ./udfNuscale.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nuscale.so ./udfNuscale.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfOffset.c -o ./udfOffset.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/offset.so ./udfOffset.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParabaloid.c -o ./udpParabaloid.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parabaloid.so ./udpParabaloid.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpParsec.cpp -o ./udpParsec.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/parsec.so ./udpParsec.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPod.c -o ./udpPod.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pod.so ./udpPod.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpPoly.c -o ./udpPoly.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/poly.so ./udpPoly.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBbox.c -o ./udfPrintBbox.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBbox.so ./udfPrintBbox.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintBrep.c -o ./udfPrintBrep.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printBrep.so ./udfPrintBrep.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfPrintEgo.c -o ./udfPrintEgo.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/printEgo.so ./udfPrintEgo.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpProp.c -o ./udpProp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/prop.so ./udpProp.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpRadwaf.c -o ./udpRadwaf.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/radwaf.so ./udpRadwaf.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSample.c -o ./udpSample.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sample.so ./udpSample.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSew.c -o ./udpSew.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/sew.so ./udpSew.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfShadow.c -o ./udfShadow.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/shadow.so ./udfShadow.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfSlices.c -o ./udfSlices.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slices.so ./udfSlices.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpStag.c -o ./udpStag.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stag.so ./udpStag.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfStiffener.c -o ./udfStiffener.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stiffener.so ./udfStiffener.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpSupell.c -o ./udpSupell.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/supell.so ./udpSupell.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udfTester1.c -o ./udfTester1.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester1.so ./udfTester1.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpTester2.c -o ./udpTester2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tester2.so ./udpTester2.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpVsp3.c -o ./udpVsp3.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vsp3.so ./udpVsp3.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWaffle.c -o ./udpWaffle.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/waffle.so ./udpWaffle.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. udpWarp.c -o ./udpWarp.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/warp.so ./udpWarp.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. eggPDT2.c -o ./eggPDT2.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/PDT2.so ./eggPDT2.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/naca456.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/naca456.so ./udpNaca456.o ./naca456.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timEreped.c -o ./timEreped.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ereped.so ./timEreped.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timMitten.c -o ./timMitten.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mitten.so ./timMitten.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlotter.c -o ./timPlotter.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plotter.so ./timPlotter.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timPlugs.c -o ./timPlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/plugs.so ./timPlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timSlugs.c -o ./timSlugs.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/slugs.so ./timSlugs.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timVspSetup.c -o ./timVspSetup.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vspSetup.so ./timVspSetup.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -locsm -lwsserver -legads -ldl -lm
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
cp -p OpenCSM.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/OpenCSM.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
cp -p common.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/common.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
cp -p udp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
cp -p esp.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/esp.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
cp -p tim.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/tim.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
cp -p egg.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/egg.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
cp -p udpUtilities.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
cp -p udpUtilities.c /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/udpUtilities.c
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/OpenCSM'
(cd Slugs; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. Tessellate.c \
-o ./Tessellate.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/Slugs ./Slugs.o ./Fitter.o ./RedBlackTree.o \
./Tessellate.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. TestFit.c -o ./TestFit.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/TestFit ./TestFit.o ./Fitter.o -lrt -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads \
-lpthread -lz -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/Slugs'
(cd CAPS; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
/bin/cp Cart3D/X86_64_GCC/libc3dio.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libc3dio.a
/bin/cp Cart3D/X86_64_GCC/libCart3D.a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libCart3D.a
/bin/cp Executables/LINUX64/avl /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/avl
/bin/cp Executables/LINUX64/pplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pplot
/bin/cp Executables/LINUX64/pxplot /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/pxplot
/bin/cp Executables/LINUX64/xfoil /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/xfoil
/bin/cp Executables/LINUX64/mastros.exe /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mastros.exe
/bin/cp Executables/LINUX64/ASTRO.D01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.D01
/bin/cp Executables/LINUX64/ASTRO.IDX /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/ASTRO.IDX
/bin/cp Executables/LINUX64/mses /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mses
/bin/cp Executables/LINUX64/mset /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/mset
/bin/cp Libraries/LINUX64/aflr2AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr2AIM.so
/bin/cp Libraries/LINUX64/aflr3AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr3AIM.so
/bin/cp Libraries/LINUX64/aflr4AIM.so /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/aflr4AIM.so
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS'
(cd CAPS/src; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
cp -p ../include/caps.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/caps.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
cp -p ../include/capsErrors.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsErrors.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
cp -p ../include/capsTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/capsTypes.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
cp -p ../include/aimUtil.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimUtil.h
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aimMesh.h
cp -p ../include/aimMesh.h /home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../include \
aimMesh.c -o ./aimMesh.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a
ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libaimUtil.a ./aimUtil.o ./aimMesh.o \
./aimTransferUtil.o
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. \
-I/usr/include/udunits2 printObject.c -o ./printObject.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcaps.so
(cd .; gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib -ludunits2 -locsm -legads -ldl \
-lrt -lm )
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libcapsstatic.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingAIM.c \
-o ./testingAIM.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingAIM.so ./testingAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include testingWriter.c \
-o ./testingWriter.o
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so
rm: cannot remove ‘/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so’: No such file or directory
make[1]: [/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so] Error 1 (ignored)
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/testingWriter.so ./testingWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include phaseUtil.c \
-o ./phaseUtil.o
gcc -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/phaseUtil ./phaseUtil.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -ludunits2 -locsm -legads -ldl -lrt -lm
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/src'
(cd ../CAPSexamples; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(make -C cCAPS -f aeroelastic_SU2.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include avlTest.c -o ./avlTest.o
gcc -g -o ./avlTest ./avlTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include awaveTest.c -o ./awaveTest.o
gcc -g -o ./awaveTest ./awaveTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include frictionTest.c -o ./frictionTest.o
gcc -g -o ./frictionTest ./frictionTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dAFLR2Test.c -o ./fun3dAFLR2Test.o
gcc -g -o ./fun3dAFLR2Test ./fun3dAFLR2Test.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fun3dTetgenTest.c -o ./fun3dTetgenTest.o
gcc -g -o ./fun3dTetgenTest ./fun3dTetgenTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aeroelasticTest.c -o ./aeroelasticTest.o
gcc -g -o ./aeroelasticTest ./aeroelasticTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmTest.c -o ./hsmTest.o
gcc -g -o ./hsmTest ./hsmTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmSimplePlateTest.c -o ./hsmSimplePlateTest.o
gcc -g -o ./hsmSimplePlateTest ./hsmSimplePlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmCantileverPlateTest.c -o ./hsmCantileverPlateTest.o
gcc -g -o ./hsmCantileverPlateTest ./hsmCantileverPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include hsmJoinedPlateTest.c -o ./hsmJoinedPlateTest.o
gcc -g -o ./hsmJoinedPlateTest ./hsmJoinedPlateTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include interferenceTest.c \
-o ./interferenceTest.o
gcc -g -o ./interferenceTest ./interferenceTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include msesTest.c -o ./msesTest.o
gcc -g -o ./msesTest ./msesTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -legads -locsm \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include mystranTest.c -o ./mystranTest.o
gcc -g -o ./mystranTest ./mystranTest.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads -ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include pointwiseTest.c -o ./pointwiseTest.o
gcc -g -o ./pointwiseTest ./pointwiseTest.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lcaps -locsm -legads \
-ludunits2 -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples'
(cd CAPS/aim; make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
make -C utils
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. vlmSpanSpace.cpp -o ./vlmSpanSpace.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a attrUtils.o meshUtils.o cfdUtils.o miscUtils.o feaUtils.o vlmUtils.o nastranUtils.o tecplotUtils.o arrayUtils.o deprecateUtils.o cardUtils.o nastranCards.o jsonUtils.o nastranOP2Reader.o vlmSpanSpace.o )
ar: creating /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libutils.a
mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils
cp -p -f attrUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrUtils.h
cp -p -f nastranCards.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranCards.h
cp -p -f cfdTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdTypes.h
cp -p -f arrayUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/arrayUtils.h
cp -p -f meshUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshUtils.h
cp -p -f feaTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaTypes.h
cp -p -f miscUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscUtils.h
cp -p -f meshTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/meshTypes.h
cp -p -f attrTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/attrTypes.h
cp -p -f vlmTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmTypes.h
cp -p -f feaUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/feaUtils.h
cp -p -f cfdUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cfdUtils.h
cp -p -f vlmUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmUtils.h
cp -p -f cardTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardTypes.h
cp -p -f jsonUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/jsonUtils.h
cp -p -f nastranUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/nastranUtils.h
cp -p -f deprecateUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/deprecateUtils.h
cp -p -f miscTypes.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/miscTypes.h
cp -p -f tecplotUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/tecplotUtils.h
cp -p -f vlmSpanSpace.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/vlmSpanSpace.h
cp -p -f cardUtils.h /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include/aim/utils/cardUtils.h
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/utils'
make -C friction
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -Wno-format -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils frictionAIM.c \
-o ./frictionAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/frictionAIM.so ./frictionAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/bin/friction ./friction.o
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/friction'
make -C tetgen
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/tetgenAIM.so ./tetgenAIM.o \
./tetgen_Interface.o ./tetgen.o \
./predicates.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -ldl -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tetgen'
make -C tacs
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils tacsAIM.c \
-o ./tacsAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tacsAIM.so ./tacsAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tacs'
make -C astros
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils astrosCards.c \
-o ./astrosCards.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/astrosAIM.so ./astrosAIM.o ./astrosUtils.o ./astrosCards.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/astros'
make -C pointwise
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils hashElement.c \
-o ./hashElement.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pointwiseAIM.so ./pointwiseAIM.o ./hashElement.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm -lpthread
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/pointwise'
make -C xfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
xfoilAIM.c -o ./xfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/xfoilAIM.so ./xfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/xfoil'
make -C aflr2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr2'
make -C aflr4
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr4'
make -C su2
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/su2'
make -C cgt
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include aflr4egads.c \
-o ./aflr4egads.o
g++ -g -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/bin/egads2cgt ./egads2cgt.o ./aflr4egads.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -legads -lcaps -locsm -lrt -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cgt'
make -C mses
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils msesUtils.c -o msesUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/msesAIM.so ./msesAIM.o ./msesUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mses'
make -C egadsTess
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils egadsTessAIM.c \
-o ./egadsTessAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/egadsTessAIM.so ./egadsTessAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/egadsTess'
make -C sierraSD
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSD'
make -C masstran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils masstranAIM.cpp \
-o ./masstranAIM.o
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/masstranAIM.so ./masstranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/masstran'
make -C plato
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/plato'
make -C refine
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 \
-I../meshWriter/libmeshbWriter/libMeshb/sources \
../meshWriter/libmeshbWriter/libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/refineAIM.so ./refineAIM.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/refine'
make -C awave
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils awaveAIM.c \
-o ./awaveAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/awaveAIM.so ./awaveAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/awave'
make -C tsfoil
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils \
tsfoilAIM.c -o ./tsfoilAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tsfoilAIM.so ./tsfoilAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/tsfoil'
make -C delaundo
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils delaundoAIM.c \
-o ./delaundoAIM.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/delaundoAIM.so ./delaundoAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl \
-lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/delaundo'
make -C abaqus
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -DHAVE_PYTHON -I/home/jenkins/util/ESP/Python/ESP_Python-3.11.9/include/python3.11 -Icython -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/abaqusAIM.so ./abaqusAIM.o ./abaqusUtils.o ./abaqusFILReader.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/abaqus'
make -C fun3d
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -DHAVE_PYTHON -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -DCYTHON_PEP489_MULTI_PHASE_INIT=0 \
-I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/fun3dAIM.so ./fun3dAIM.o ./fun3dUtils.o \
./fun3dNamelist.o -L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/fun3d'
make -C cbaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I. -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/cbaeroAIM.so -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cbaero'
make -C interference
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. cloudFns.c \
-o ./cloudFns.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/interferenceAIM.so \
./interferenceAIM.o ./cloudFns.o -L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib \
-laimUtil -locsm -legads -ludunits2 -ldl -lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/interference'
make -C meshWriter
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter'
make -C libmeshbWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -IlibMeshb/sources -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include libMeshb/sources/libmeshb7.c \
-o ./libmeshb7.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libmeshbWriter.so ./libmeshbWriter.o ./libmeshb7.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/libmeshbWriter'
make -C fastWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include fastWriter.c \
-o ./fastWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/fastWriter.so ./fastWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/fastWriter'
make -C tecplotWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include tecplotWriter.c \
-o ./tecplotWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/tecplotWriter.so ./tecplotWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/tecplotWriter'
make -C vtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include vtkWriter.c \
-o ./vtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/vtkWriter.so ./vtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/vtkWriter'
make -C bstlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bstlWriter.c \
-o ./bstlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bstlWriter.so ./bstlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bstlWriter'
make -C bvtkWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include bvtkWriter.c \
-o ./bvtkWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/bvtkWriter.so ./bvtkWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/bvtkWriter'
make -C su2Writer
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include su2Writer.c \
-o ./su2Writer.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/su2Writer.so ./su2Writer.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/su2Writer'
make -C stlWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include stlWriter.c \
-o ./stlWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/stlWriter.so ./stlWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/stlWriter'
make -C ugridWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I../include -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include ugridWriter.c \
-o ./ugridWriter.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/ugridWriter.so ./ugridWriter.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -laimUtil -legads -locsm -ludunits2 -ldl -lrt -lm
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/ugridWriter'
make -C exodusWriter
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[3]: Nothing to be done for `default'.
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/meshWriter/exodusWriter'
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
XML developer libarary missing. Not compiling cart3dAIM.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/cart3d'
make -C nastran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils nastranAIM.c \
-o ./nastranAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/nastranAIM.so ./nastranAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/nastran'
make -C spinnaker
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/spinnaker'
make -C aflr3
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/aflr3'
make -C sierraSM
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/sierraSM'
make -C hsm
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 \
-o src/rcm.o
g++ -g -c -O -fPIC -DOCC_CONVERT_SIGNALS -D_GNU_SOURCE=1 -DNDEBUG -DNo_Exception -D_OCC64 -Wall -Wno-dangling-else -Wno-parentheses -Wno-unused-result -Wno-format-truncation -std=c++11 rcm/genrcmi.cpp -DREVISION=7.8 \
-o src/genrcmi.o
make -C src hsmglr.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmbb2.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmre1.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmdep.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrfm.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmout.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmren.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmprj.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src atanc.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src cross.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src ludcmp.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmabd.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src bmdump.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmrun.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmeqn.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmsol.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src hsmgeo.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src sbsolve.o
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
make -C src /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/libhsm.a
(cd .; ar -rs /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/libhsm.a
make[3]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm/src'
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/hsmAIM.so
gfortran -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm \
-legads -ludunits2 -lhsm -ldl -lstdc++
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/hsm'
make -C avl
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/avlAIM.so
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib -laimUtil -lutils -locsm -legads -ludunits2 -ldl \
-lstdc++ -lrt -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/avl'
make -C custom
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make[2]: Nothing to be done for `default'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/custom'
make -C skeleton
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils skeletonAIM.c \
-o ./skeletonAIM.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/skeletonAIM.so ./skeletonAIM.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -ldl -lm
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/skeleton'
make -C unitTest
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make[2]: Nothing to be done for `all'.
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/unitTest'
make -C mystran
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils mystranUtils.c \
-o ./mystranUtils.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/mystranAIM.so ./mystranAIM.o ./mystranUtils.o \
-L/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/src/CAPS/aim/mystran'
make -C zaero
make[2]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I../utils zaeroGraphical.c -o zaeroGraphical.o
gcc -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib -lutils -laimUtil -locsm -legads -ludunits2 -lm -ldl
make[2]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim/zaero'
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/src/CAPS/aim'
(cd OpenCSM; make -f serveESP.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timCapsMode.c -o ./timCapsMode.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/capsMode.so ./timCapsMode.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timFlowchart.c -o ./timFlowchart.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/flowchart.so ./timFlowchart.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/include -I. timViewer.c -o ./timViewer.o
touch /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/viewer.so ./timViewer.o -L/home/jenkins/workspace/ESP_Beta/7.8/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=7.8 -I/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/EngSketchPad/lib/pyscript.so
rm /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/lib/pyscript.so
g++ -g -shared -Wl,-no-undefined -o /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/LINUX64/EngSketchPad/src/OpenCSM'
*** Build Completed! ***
+ export CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ CSMDATA=/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data
+ cd /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/Verification.sh
+ bash -ex /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/Verification.sh
+ expectSuccess 01 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/expressions
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/expressions.vfy", so verification is being skipped
ERROR:: problem evaluating argument 2 (slice(e3,0,999)) for Branch 152 (set)
ERROR:: problem evaluating argument 2 (slice(e3,14,999)) for Branch 158 (set)
ERROR:: problem evaluating argument 2 (slice(e3,4,-1)) for Branch 164 (set)
==> serveESP completed successfully with no verification data
real 0m0.105s
user 0m0.090s
sys 0m0.014s
+ set +x
=============================================
ESP verification case 01 passed (as expected)
=============================================
+ expectSuccess 02 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/demo2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/demo2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.367s
user 0m0.476s
sys 0m0.029s
+ set +x
=============================================
ESP verification case 02 passed (as expected)
=============================================
+ expectSuccess 03 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial1_whole
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial1_whole.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m2.932s
user 0m4.364s
sys 0m0.103s
+ set +x
=============================================
ESP verification case 03 passed (as expected)
=============================================
+ expectSuccess 04 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.548s
user 0m0.751s
sys 0m0.032s
+ set +x
=============================================
ESP verification case 04 passed (as expected)
=============================================
+ expectSuccess 05 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/design3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/design3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.524s
user 0m0.723s
sys 0m0.023s
+ set +x
=============================================
ESP verification case 05 passed (as expected)
=============================================
+ expectSuccess 06 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.443s
user 0m0.847s
sys 0m0.027s
+ set +x
=============================================
ESP verification case 06 passed (as expected)
=============================================
+ expectSuccess 07 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/tutorial3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/legacy/verify_7.8.0/tutorial3.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m3.548s
user 0m5.647s
sys 0m0.121s
+ set +x
=============================================
ESP verification case 07 passed (as expected)
=============================================
+ expectSuccess 08 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/myPlane
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/CAPS/verify_7.8.0/myPlane.vfy", so verification is being skipped
==> serveESP completed successfully with 12 warnings and no verification data
real 0m27.363s
user 0m46.139s
sys 0m0.628s
+ set +x
=============================================
ESP verification case 08 passed (as expected)
=============================================
+ expectSuccess 09 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/bottle
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/verify_7.8.0/bottle.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.584s
user 0m0.836s
sys 0m0.034s
+ set +x
=============================================
ESP verification case 09 passed (as expected)
=============================================
+ expectSuccess 10 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/wingMultiModel
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/wingMultiModel.vfy", so verification is being skipped
==> serveESP completed successfully with 4 warnings and no verification data
real 0m35.052s
user 0m59.935s
sys 0m2.859s
+ set +x
=============================================
ESP verification case 10 passed (as expected)
=============================================
+ expectSuccess 11 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/bullet
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/bullet.vfy", so verification is being skipped
WARNING:: 8 _hist and/or __trace__ attributes removed
WARNING:: 8 _hist and/or __trace__ attributes removed
==> serveESP completed successfully with 1 warnings and no verification data
real 0m0.376s
user 0m0.412s
sys 0m0.032s
+ set +x
=============================================
ESP verification case 11 passed (as expected)
=============================================
+ expectSuccess 12 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/connect5
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/connect5.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.581s
user 0m0.921s
sys 0m0.022s
+ set +x
=============================================
ESP verification case 12 passed (as expected)
=============================================
+ expectSuccess 13 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/group2
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/group2.vfy", so verification is being skipped
==> serveESP completed successfully with no verification data
real 0m0.161s
user 0m0.255s
sys 0m0.021s
+ set +x
=============================================
ESP verification case 13 passed (as expected)
=============================================
+ expectSuccess 14 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
+ ./serveESP -batch -verify -outLevel 0 /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/csm3
WARNING:: cannot open "/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/basic/verify_7.8.0/csm3.vfy", so verification is being skipped
nnode=8
nedge=12
nface=6
nnode=8
nedge=12
nface=6
nnode=16
nedge=24
nface=10
nnode=8
nedge=12
nface=6
==> serveESP completed successfully with no verification data
real 0m0.471s
user 0m0.593s
sys 0m0.025s
+ set +x
=============================================
ESP verification case 14 passed (as expected)
=============================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/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 71 tests in 2.256s
OK
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/pyESP/testOCSM
+ source /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/test_pyOCSM.sh
++ set -x
++ python -u test_pyOCSM.py -skipHelp
real 0m6.227s
user 0m11.928s
sys 0m0.163s
++ set +x
=================================================
test_pyOCSM.py passed (as expected)
=================================================
+ cd /home/jenkins/workspace/ESP_Beta/7.8/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 14.659s
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/7.8/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 2244 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 2244 2244
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 450 902
AFLR2 IG : Nodes, Faces = 900 1802
AFLR2 IG : Nodes, Faces = 1145 2292
AFLR2 IG : Nodes, Faces = 1260 2522
AFLR2 IG : Nodes, Faces = 1350 2702
AFLR2 IG : Nodes, Faces = 1360 2722
AFLR2 IG : Nodes, Faces = 1460 2922
AFLR2 IG : Nodes, Faces = 1560 3122
AFLR2 IG : Nodes, Faces = 1660 3322
AFLR2 IG : Nodes, Faces = 1760 3522
AFLR2 IG : Nodes, Faces = 1800 3602
AFLR2 IG : Nodes, Faces = 1860 3722
AFLR2 IG : Nodes, Faces = 1960 3922
AFLR2 IG : Nodes, Faces = 2060 4122
AFLR2 IG : Nodes, Faces = 2085 4172
AFLR2 IG : Nodes, Faces = 2244 4490
AFLR2 IG : Nodes, Faces = 2248 4490
AFLR2 IG : Nodes, Faces = 2244 2244
AFLR2 : CPU Time = 0.052 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 = 0.159 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.015 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 = 0.098 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.005 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 23187
Number of elements = 46374
Number of tris = 44150
Number of quad = 0
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 = 0.030 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 = 0.091 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.006 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 = 0.096 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 23187 44150
AFLR2 : CPU Time = 0.022 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 = 0.084 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 = 0.123 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 29897 57550
AFLR2 : CPU Time = 0.009 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 = 0.012 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 4705 9066
AFLR2 : CPU Time = 0.002 seconds
AFLR2 : DONE
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 4705
Number of elements = 9410
Number of tris = 9066
Number of quad = 0
Writing 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 = 0.019 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 = 0.010 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 = 0.007 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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
AFLR2 : ---------------------------------------
AFLR2 : AFLR2 LIBRARY
AFLR2 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR2 : TRIA/QUAD GRID GENERATOR
AFLR2 : Version Number 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1189
Number of elements = 6249
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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:62030)
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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 16488
Number of elements = 93795
Number of triangles = 7926
Number of quadrilatarals = 0
Number of tetrahedrals = 85869
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_box (test_aflr3.TestAFLR3.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2589
Number of elements = 13809
Number of triangles = 2758
Number of quadrilatarals = 0
Number of tetrahedrals = 11051
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_boxhole (test_aflr3.TestAFLR3.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4694
Number of elements = 25935
Number of triangles = 3326
Number of quadrilatarals = 0
Number of tetrahedrals = 22609
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_cylinder (test_aflr3.TestAFLR3.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5554
Number of elements = 30862
Number of triangles = 3756
Number of quadrilatarals = 0
Number of tetrahedrals = 27106
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch (test_aflr3.TestAFLR3.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2260
Number of elements = 12133
Number of triangles = 2222
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2392
Number of elements = 12577
Number of triangles = 2666
Number of quadrilatarals = 0
Number of tetrahedrals = 9911
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3341
Number of elements = 18069
Number of triangles = 3110
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 3606
Number of elements = 18961
Number of triangles = 4002
Number of quadrilatarals = 0
Number of tetrahedrals = 14959
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4414
Number of elements = 23974
Number of triangles = 3998
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 4)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 4811
Number of elements = 25310
Number of triangles = 5334
Number of quadrilatarals = 0
Number of tetrahedrals = 19976
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 4):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 4):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 4):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 4)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 4):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 5490
Number of elements = 29891
Number of triangles = 4886
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6019
Number of elements = 31671
Number of triangles = 6666
Number of quadrilatarals = 0
Number of tetrahedrals = 25005
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 6542
Number of elements = 35667
Number of triangles = 5774
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 6)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7203
Number of elements = 37891
Number of triangles = 7998
Number of quadrilatarals = 0
Number of tetrahedrals = 29893
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 6):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 6):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 6):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 6):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 6):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 6)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 6):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 7601
Number of elements = 41489
Number of triangles = 6662
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 7)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8394
Number of elements = 44157
Number of triangles = 9330
Number of quadrilatarals = 0
Number of tetrahedrals = 34827
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 7):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 7):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 7):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 7):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 7):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 7):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 7):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 19800
Number of elements = 109798
Number of triangles = 15540
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 6 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 7 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 8 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 9 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 10 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 11 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 12 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 13 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 14 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 15 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 16 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 17 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 18 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 19 (of 19)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 22741
Number of elements = 119570
Number of triangles = 25312
Number of quadrilatarals = 0
Number of tetrahedrals = 94258
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 19):
Number of nodes = 1208
Number of elements = 6360
Number of triangles = 1334
Number of quadrilatarals = 0
Number of tetrahedrals = 5026
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 19):
Number of nodes = 1184
Number of elements = 6217
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4885
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 19):
Number of nodes = 1214
Number of elements = 6384
Number of triangles = 1336
Number of quadrilatarals = 0
Number of tetrahedrals = 5048
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 4 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 19):
Number of nodes = 1205
Number of elements = 6349
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5017
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 19):
Number of nodes = 1208
Number of elements = 6361
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5029
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 6 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 6 (of 19):
Number of nodes = 1184
Number of elements = 6220
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4888
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 7 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 7 (of 19):
Number of nodes = 1191
Number of elements = 6266
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4934
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 8 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 8 (of 19):
Number of nodes = 1193
Number of elements = 6272
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4940
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 9 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 9 (of 19):
Number of nodes = 1176
Number of elements = 6165
Number of triangles = 1330
Number of quadrilatarals = 0
Number of tetrahedrals = 4835
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 10 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 10 (of 19):
Number of nodes = 1203
Number of elements = 6314
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4982
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 11 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 11 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 12 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 12 (of 19):
Number of nodes = 1192
Number of elements = 6269
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4937
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 13 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 13 (of 19):
Number of nodes = 1198
Number of elements = 6296
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4964
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 14 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 14 (of 19):
Number of nodes = 1223
Number of elements = 6443
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 5111
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 15 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 15 (of 19):
Number of nodes = 1184
Number of elements = 6224
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4892
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 16 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 16 (of 19):
Number of nodes = 1195
Number of elements = 6287
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4955
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 17 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 17 (of 19):
Number of nodes = 1197
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 18 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 18 (of 19):
Number of nodes = 1203
Number of elements = 6310
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4978
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 19 (of 19)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 19 (of 19):
Number of nodes = 1191
Number of elements = 6253
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4921
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_faceMatch_MultiDomain (test_aflr3.TestAFLR3.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8857
Number of elements = 49191
Number of triangles = 6284
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 8989
Number of elements = 49635
Number of triangles = 6728
Number of quadrilatarals = 0
Number of tetrahedrals = 42907
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 7796
Number of elements = 43368
Number of triangles = 5396
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 1193
Number of elements = 6267
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4935
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9944
Number of elements = 55193
Number of triangles = 7174
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10218
Number of elements = 56081
Number of triangles = 8062
Number of quadrilatarals = 0
Number of tetrahedrals = 48019
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7818
Number of elements = 43469
Number of triangles = 5398
Number of quadrilatarals = 0
Number of tetrahedrals = 38071
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1202
Number of elements = 6320
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4988
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 1198
Number of elements = 6292
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4960
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9609
Number of elements = 53228
Number of triangles = 6994
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9829
Number of elements = 53956
Number of triangles = 7722
Number of quadrilatarals = 0
Number of tetrahedrals = 46234
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7789
Number of elements = 43295
Number of triangles = 5394
Number of quadrilatarals = 0
Number of tetrahedrals = 37901
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1186
Number of elements = 6230
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4898
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 854
Number of elements = 4431
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3435
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9348
Number of elements = 51734
Number of triangles = 6812
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9531
Number of elements = 52330
Number of triangles = 7408
Number of quadrilatarals = 0
Number of tetrahedrals = 44922
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7804
Number of elements = 43358
Number of triangles = 5386
Number of quadrilatarals = 0
Number of tetrahedrals = 37972
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 1200
Number of elements = 6311
Number of triangles = 1332
Number of quadrilatarals = 0
Number of tetrahedrals = 4979
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9183
Number of elements = 50871
Number of triangles = 6632
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 9322
Number of elements = 51307
Number of triangles = 7068
Number of quadrilatarals = 0
Number of tetrahedrals = 44239
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7927
Number of elements = 44116
Number of triangles = 5382
Number of quadrilatarals = 0
Number of tetrahedrals = 38734
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 868
Number of elements = 4530
Number of triangles = 996
Number of quadrilatarals = 0
Number of tetrahedrals = 3534
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 527
Number of elements = 2661
Number of triangles = 690
Number of quadrilatarals = 0
Number of tetrahedrals = 1971
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10181
Number of elements = 56797
Number of triangles = 6782
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 10671
Number of elements = 58561
Number of triangles = 8546
Number of quadrilatarals = 0
Number of tetrahedrals = 50015
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 7741
Number of elements = 43010
Number of triangles = 5362
Number of quadrilatarals = 0
Number of tetrahedrals = 37648
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 2692
Number of elements = 14435
Number of triangles = 2800
Number of quadrilatarals = 0
Number of tetrahedrals = 11635
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 238
Number of elements = 1116
Number of triangles = 384
Number of quadrilatarals = 0
Number of tetrahedrals = 732
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1500
Number of elements = 7757
Number of triangles = 1986
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 3)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 1564
Number of elements = 7881
Number of triangles = 2110
Number of quadrilatarals = 0
Number of tetrahedrals = 5771
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 3):
Number of nodes = 1160
Number of elements = 6087
Number of triangles = 1308
Number of quadrilatarals = 0
Number of tetrahedrals = 4779
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 3):
Number of nodes = 360
Number of elements = 1635
Number of triangles = 718
Number of quadrilatarals = 0
Number of tetrahedrals = 917
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 3):
Number of nodes = 44
Number of elements = 159
Number of triangles = 84
Number of quadrilatarals = 0
Number of tetrahedrals = 75
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 3 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 4 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 5 (of 5)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 5):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 5):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 3 (of 5):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 4 (of 5):
Number of nodes = 711
Number of elements = 3685
Number of triangles = 844
Number of quadrilatarals = 0
Number of tetrahedrals = 2841
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 5 (of 5):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Getting volume mesh for body 2 (of 2)
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 1 (of 2):
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh for body 2 (of 2):
Number of nodes = 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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_aflr3.TestAFLR3.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_reenter (test_aflr3.TestAFLR3.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2940
Number of elements = 12771
Number of triangles = 5452
Number of quadrilatarals = 0
Number of tetrahedrals = 7319
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 2497
Number of elements = 10947
Number of triangles = 4552
Number of quadrilatarals = 0
Number of tetrahedrals = 6395
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60311
Number of elements = 351913
Number of triangles = 12928
Number of quadrilatarals = 0
Number of tetrahedrals = 338985
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 59175
Number of elements = 344623
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 332195
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
Getting mesh sizing parameters
Mesh sizing name - Wake
Done getting mesh sizing parameters
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 60311
Number of elements = 351413
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 338985
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_MultiBody_quad (test_aflr4.TestAFLR4.test_MultiBody_quad) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
ok
test_SingleBody_output (test_aflr4.TestAFLR4.test_SingleBody_output) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - trailingEdge
Done getting mesh sizing parameters
ok
test_all (test_aflr4.TestAFLR4.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 8
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Name = farfield, index = 8
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_box (test_aflr4.TestAFLR4.test_box) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_boxhole (test_aflr4.TestAFLR4.test_boxhole) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = boxhole, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_bullet (test_aflr4.TestAFLR4.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_aflr4.TestAFLR4.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_aflr4.TestAFLR4.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch (test_aflr4.TestAFLR4.test_faceMatch) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = wall, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_faceMatch_MultiDomain (test_aflr4.TestAFLR4.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Writing Tecplot file ....
Finished writing Tecplot file
Writing Tecplot file ....
Finished writing Tecplot file
ok
test_invalid_Mesh_Lenght_Scale (test_aflr4.TestAFLR4.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_aflr4.TestAFLR4.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
ok
test_phase (test_aflr4.TestAFLR4.test_phase) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
ok
test_reenter (test_aflr4.TestAFLR4.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Writing 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_setInput (test_aflr4.TestAFLR4.test_setInput) ... EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
ok
test_sphere (test_aflr4.TestAFLR4.test_sphere) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = sphere, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_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 = 2
Name = Wing1, index = 1
Name = trailingEdge, index = 2
Writing FAST file ....
Finished writing FAST file
Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_Output_v6 (test_cbaero.TestCBAERO.test_Output_v6) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_inputs (test_cbaero.TestCBAERO.test_inputs) ... Writing CBAero input file - cbaero_CAPS.cbaero
Writing CBAero tagged regions - TaggedRegions
Writing CBAero setup file - cbaero_CAPS.stp
ok
test_MultiBody (test_egadsTess.TestEGADS.test_MultiBody) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 4
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Wake, index = 3
Name = Farfield, index = 4
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_SingleBody_AnalysisOutVal (test_egadsTess.TestEGADS.test_SingleBody_AnalysisOutVal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
ok
test_all (test_egadsTess.TestEGADS.test_all) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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
7FEF57FFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FEF57FFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FEF7FA4A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FEF7FA4A740 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
7FEF5D466700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FEF5D466700 EGADS Info: 7FEF5CC65700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FEF5CC65700 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
7FEF5CC65700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FEF5CC65700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FEF7FA4A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FEF7FA4A740 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
7FEF57FFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FEF57FFF700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
7FEF5D466700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FEF5D466700 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
ok
test_bullet (test_egadsTess.TestEGADS.test_bullet) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = bullet, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cone (test_egadsTess.TestEGADS.test_cone) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cone, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_cylinder (test_egadsTess.TestEGADS.test_cylinder) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = cylinder, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
ok
test_invalid_Mesh_Lenght_Scale (test_egadsTess.TestEGADS.test_invalid_Mesh_Lenght_Scale) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
ok
test_journal (test_egadsTess.TestEGADS.test_journal) ... ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
CAPS Info: Hit last success -- going live!
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:62030)
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:62030)
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:62030)
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:62030)
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:62030)
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:62030)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box, index = 1
Name = farfield, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 1
Name = box, index = 1
Getting mesh sizing parameters
Mesh sizing name - box
Done getting mesh sizing parameters
ok
test_reenter (test_egadsTess.TestEGADS.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing 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 = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Writing 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 = 7766
Number of elements = 15528
Number of triangle elements = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5870
Number of elements = 11736
Number of triangle elements = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14124
Total number of elements = 28236
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.16
Creating surface mesh ...
Surface mesh seconds: 0.04
Recovering boundaries...
Boundary recovery seconds: 0.19
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.08
Recovering Delaunayness...
Delaunay recovery seconds: 0.08
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 3.01
Smoothing vertices...
Mesh smoothing seconds: 2.96
Improving mesh...
Mesh improvement seconds: 0.06
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.02
Total running seconds: 6.61
Statistics:
Input points: 14124
Input facets: 28236
Input segments: 42354
Input holes: 2
Input regions: 0
Mesh points: 33059
Mesh tetrahedra: 159851
Mesh faces: 333820
Mesh faces on exterior boundary: 28236
Mesh faces on input facets: 28236
Mesh edges on input segments: 42354
Steiner points inside domain: 18935
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 5
Design Variable name - Mach
Warning: No initial value set for Mach
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_Design_Sensitivity (test_fun3d.TestFUN3D.test_Design_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - Alpha
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Creating FUN3D directory tree
DesignVariable = Alpha
Writing rubber.data
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Overwrite_NML is set to 'True' - a new namelist will be created
Creating namelist
Done writing nml file with Python
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_Mesh_Morph_Sensitivity (test_fun3d.TestFUN3D.test_Mesh_Morph_Sensitivity) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 6
Design Variable name - Alpha
Design Variable name - Beta
Warning: No initial value set for Beta
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Getting CFD functional.......
Number of design variables - 2
Objective name - Composite
Objective name - Lift^2
Done getting CFD functional
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing rubber.data
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
Projecting tessellation 1 (of 3) on to new body
Projecting tessellation 2 (of 3) on to new body
Projecting tessellation 3 (of 3) on to new body
Python library was linked, but will not be used!
Creating FUN3D directory tree
DesignVariable = Alpha
DesignVariable = Beta
DesignVariable = area
DesignVariable = aspect
DesignVariable = taper
DesignVariable = twist
Writing sensitivity file for body 1, File - Rubberize/model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize/model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize/model.tec.3.sd1
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing surface file for 1 (of 3) in body 1 File - Flow/fun3d_CAPS_body1.dat
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Reading rubber.data
ok
test_cythonNML (test_fun3d.TestFUN3D.test_cythonNML) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 7766
Number of elements = 15528
Number of triangle elements = 15528
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 5870
Number of elements = 11736
Number of triangle elements = 11736
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 14124
Total number of elements = 28236
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000T1.00e-16A
Delaunizing vertices...
Delaunay seconds: 0.15
Creating surface mesh ...
Surface mesh seconds: 0.04
Recovering boundaries...
Boundary recovery seconds: 0.17
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0.07
Recovering Delaunayness...
Delaunay recovery seconds: 0.08
Refining mesh...
18827 insertions, added 13420 points, 721721 tetrahedra in queue.
6269 insertions, added 2485 points, 625204 tetrahedra in queue.
8356 insertions, added 2101 points, 168215 tetrahedra in queue.
Refinement seconds: 3.06
Smoothing vertices...
Mesh smoothing seconds: 2.81
Improving mesh...
Mesh improvement seconds: 0.06
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0.02
Total running seconds: 6.46
Statistics:
Input points: 14124
Input facets: 28236
Input segments: 42354
Input holes: 2
Input regions: 0
Mesh points: 33059
Mesh tetrahedra: 159851
Mesh faces: 333820
Mesh faces on exterior boundary: 28236
Mesh faces on input facets: 28236
Mesh edges on input segments: 42354
Steiner points inside domain: 18935
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing MAPBC file ....
Finished writing MAPBC file
Using Python to write FUN3D namelist (fun3d.nml)
Reading /home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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/7.8/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 - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 5043, elements - 10074
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
Python library was linked, but will not be used!
Creating FUN3D directory tree
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - area
Design Variable name - aspect
Design Variable name - taper
Design Variable name - twist
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
ok
test_moving_body (test_fun3d.TestFUN3D.test_moving_body) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Writing moving_body.input
ok
test_overwriteNML (test_fun3d.TestFUN3D.test_overwriteNML) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_phase (test_fun3d.TestFUN3D.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Number of surface: nodes - 14124, elements - 28236
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_reenter (test_fun3d.TestFUN3D.test_reenter) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Info: No recognized data transfer names found.
ok
test_symmetry (test_fun3d.TestFUN3D.test_symmetry) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Python library was linked, but will not be used!
Writing MAPBC file ....
Finished writing MAPBC file
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
Info: No recognized data transfer names found.
ok
test_box1 (test_masstran.TestMasstran.test_box1) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box2 (test_masstran.TestMasstran.test_box2) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Projecting tessellation 1 (of 1) on to new body
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 1692
Number of elements = 3380
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 3380
Elemental Quad4 = 0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_box3 (test_masstran.TestMasstran.test_box3) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - box2
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = box2, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2402
Number of elements = 2400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 2400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Design_Variable_Relation name - thick_box2
Number of design variable relations - 4
Done getting FEA design variables
ok
test_journal (test_masstran.TestMasstran.test_journal) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Updating mesh element types based on properties input
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4009
Number of elements = 8014
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 8014
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6178
Combined Number of elements = 12347
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12346
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
CAPS Info: Hit last success -- going live!
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 2168
Number of elements = 4332
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 4332
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 4000
Number of elements = 7996
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 7996
Elemental Quad4 = 0
Setting FEA Data
Mesh for body = 2
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 6169
Combined Number of elements = 12329
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 12328
Combined Elemental Quad4 = 0
Getting FEA materials.......
Number of materials - 2
Material name - madeupium
Material name - unobtainium
Done getting FEA materials
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
ok
test_plate (test_masstran.TestMasstran.test_plate) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 1
Property name - box1
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box1, index = 1
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 3
Done getting FEA design variables
ok
test_plate_point (test_masstran.TestMasstran.test_plate_point) ... Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Getting FEA properties.......
Number of properties - 2
Property name - box1
Property name - point
Done getting FEA properties
Updating mesh element types based on properties input
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 7
Design_Variable name - H
Design_Variable name - L
Design_Variable name - W
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> L
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> W
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> H
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
===> x0
Mapping Csys attributes ................
Number of unique Csys attributes = 0
Getting FEA coordinate systems.......
Number of coordinate systems - 0
No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
Number of unique capsConnect attributes = 0
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = box1, index = 1
Name = point, index = 2
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 3 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 4 of face 1, unable to assign a boundary index value
Setting FEA Data
Mesh for body = 0
Number of nodal coordinates = 441
Number of elements = 400
Elemental Nodes = 0
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 400
Setting FEA Data
Mesh for body = 1
Number of nodal coordinates = 1
Number of elements = 1
Elemental Nodes = 1
Elemental Rods = 0
Elemental Tria3 = 0
Elemental Quad4 = 0
Combining multiple FEA meshes!
Combined Number of nodal coordinates = 442
Combined Number of elements = 401
Combined Elemental Nodes = 1
Combined Elemental Rods = 0
Combined Elemental Tria3 = 0
Combined Elemental Quad4 = 400
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> x1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m0
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
===> m1
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
Updating mesh element types based on properties input
Getting FEA design variables.......
Number of design variables - 4
Design_Variable name - m0
Design_Variable name - m1
Design_Variable name - x0
Design_Variable name - x1
Design_Variable_Relation name - mass_point
Design_Variable_Relation name - rho_madeupium
Name madeupium not found in attribute map!!!!
Design_Variable_Relation name - rho_unobtainium
Name unobtainium not found in attribute map!!!!
Design_Variable_Relation name - thick_box1
Number of design variable relations - 4
Done getting FEA design variables
ok
test_Cheby_Modes (test_mses.TestMSES_Kulfan.test_Cheby_Modes) ...
Getting CFD design variables.......
Number of design variables - 4
Design Variable name - alowervar
Design Variable name - auppervar
Design Variable name - classvar
Design Variable name - ztailvar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_Kulfan.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - avar
Done getting CFD design variables
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
CAPS Info: Sensitivity FD step 1.000000e-05
ok
test_allInputs (test_mses.TestMSES_Kulfan.test_allInputs) ... ok
test_execute (test_mses.TestMSES_Kulfan.test_execute) ... ok
test_sensitivity_AnalysisIn (test_mses.TestMSES_Kulfan.test_sensitivity_AnalysisIn) ... ok
test_Cheby_Modes_Symmetric (test_mses.TestMSES_NACA.test_Cheby_Modes_Symmetric) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_geom_sensitivity_CL (test_mses.TestMSES_NACA.test_geom_sensitivity_CL) ...
Getting CFD design variables.......
Number of design variables - 2
Design Variable name - camber
Design Variable name - thick
Done getting CFD design variables
ok
test_journal (test_mses.TestMSES_NACA.test_journal) ...
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
CAPS Info: Hit last success -- going live!
Getting CFD design variables.......
Number of design variables - 1
Design Variable name - thick
Done getting CFD design variables
ok
test_MultiBody (test_pointwise.TestPointwise.test_MultiBody) ... 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 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : EGADS CAD Geometry Setup
EGADS : Model has 3 Active Bodies
EGADS : Body 0 is a SolidBody
EGADS : Body 0 has 1 Shells
EGADS : Body 0 has 8 Faces
EGADS : Body 0 has 15 Edges
EGADS : Body 0 has 8 Loops
EGADS : Body 0 has 9 Nodes
EGADS : Body 1 is a SolidBody
EGADS : Body 1 has 1 Shells
EGADS : Body 1 has 8 Faces
EGADS : Body 1 has 15 Edges
EGADS : Body 1 has 8 Loops
EGADS : Body 1 has 9 Nodes
EGADS : Body 2 is a SolidBody
EGADS : Body 2 has 1 Shells
EGADS : Body 2 has 2 Faces
EGADS : Body 2 has 6 Edges
EGADS : Body 2 has 2 Loops
EGADS : Body 2 has 2 Nodes
EGADS : Check Grid BCs
EGADS : Grid BCs are OK
EGADS : Face Neighbor-Faces Information
EGADS : QC = Face Quad Combination Flag
EGADS : IER = Face Isolated Edge Refinement Flag
EGADS : ER = Face Edge Refinement Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : SF = Face Scale Factor
EGADS : Not applicable for Faces with a FarField Grid BC.
EGADS : Face Body QC IER ER Scale Neighbor
EGADS : ID Active ID Flag Flag Weight Factor Faces
EGADS : 1 Yes 0 0 1 1 1 2 3 4 5
EGADS : 2 Yes 0 0 1 1 1 1 3 4 6
EGADS : 3 Yes 0 0 1 1 1 1 2 4 7
EGADS : 4 Yes 0 0 1 1 1 1 2 3
EGADS : 5 Yes 0 0 1 1 1 1 6 7 8
EGADS : 6 Yes 0 0 1 1 1 2 5 7 8
EGADS : 7 Yes 0 0 1 1 1 3 5 6 8
EGADS : 8 Yes 0 0 1 1 1 5 6 7
EGADS : 9 Yes 1 0 1 0 10 10 11 12 13
EGADS : 10 Yes 1 0 1 0 10 9 11 12 14
EGADS : 11 Yes 1 0 1 0 10 9 10 12 15
EGADS : 12 Yes 1 0 1 0 10 9 10 11
EGADS : 13 Yes 1 0 1 0 10 9 14 15 16
EGADS : 14 Yes 1 0 1 0 10 10 13 15 16
EGADS : 15 Yes 1 0 1 0 10 11 13 14 16
EGADS : 16 Yes 1 0 1 0 10 13 14 15
EGADS : 17 Yes 2 0 1 NA NA 18
EGADS : 18 Yes 2 0 1 NA NA 17
EGADS : Face Edges Information
EGADS : Face Edges
EGADS : 1 1 4 -3 -2
EGADS : 2 3 7 -6 -5
EGADS : 3 6 9 -1 -8
EGADS : 4 -4 -9 -7
EGADS : 5 -10 2 11 -12
EGADS : 6 -11 5 13 -14
EGADS : 7 -13 8 10 -15
EGADS : 8 12 14 15
EGADS : 9 16 19 -18 -17
EGADS : 10 18 22 -21 -20
EGADS : 11 21 24 -16 -23
EGADS : 12 -19 -24 -22
EGADS : 13 -25 17 26 -27
EGADS : 14 -26 20 28 -29
EGADS : 15 -28 23 25 -30
EGADS : 16 27 29 30
EGADS : 17 -31 -32 33 34
EGADS : 18 -35 -34 36 32
EGADS : Face Loops Information
EGADS : Face Loops
EGADS : 1 1
EGADS : 2 2
EGADS : 3 3
EGADS : 4 4
EGADS : 5 5
EGADS : 6 6
EGADS : 7 7
EGADS : 8 8
EGADS : 9 9
EGADS : 10 10
EGADS : 11 11
EGADS : 12 12
EGADS : 13 13
EGADS : 14 14
EGADS : 15 15
EGADS : 16 16
EGADS : 17 17
EGADS : 18 18
EGADS : Loop Edges Information
EGADS : Loop Active Edges
EGADS : 1 Yes 1 4 -3 -2
EGADS : 2 Yes 3 7 -6 -5
EGADS : 3 Yes 6 9 -1 -8
EGADS : 4 Yes -4 -9 -7
EGADS : 5 Yes -10 2 11 -12
EGADS : 6 Yes -11 5 13 -14
EGADS : 7 Yes -13 8 10 -15
EGADS : 8 Yes 12 14 15
EGADS : 9 Yes 16 19 -18 -17
EGADS : 10 Yes 18 22 -21 -20
EGADS : 11 Yes 21 24 -16 -23
EGADS : 12 Yes -19 -24 -22
EGADS : 13 Yes -25 17 26 -27
EGADS : 14 Yes -26 20 28 -29
EGADS : 15 Yes -28 23 25 -30
EGADS : 16 Yes 27 29 30
EGADS : 17 Yes -31 -32 33 34
EGADS : 18 Yes -35 -34 36 32
EGADS : Edge Node, Scale Factor, and Neighbor-Faces Information
EGADS : ESF = Edge Scale Factor
EGADS : Not applicable for DEGENERATE Edges or Edges with a FarField
EGADS : Grid BC Neighbor Face.
EGADS : Neighbor
EGADS : Edge Body Active Node1 Node2 ESF Faces
EGADS : 1 0 Yes 1 2 1 1 3
EGADS : 2 0 Yes 1 3 1 1 5
EGADS : 3 0 Yes 3 4 1 1 2
EGADS : 4 0 Yes 2 4 1 1 4
EGADS : 5 0 Yes 3 5 1 2 6
EGADS : 6 0 Yes 5 6 1 2 3
EGADS : 7 0 Yes 4 6 1 2 4
EGADS : 8 0 Yes 5 1 1 3 7
EGADS : 9 0 Yes 6 2 1 3 4
EGADS : 10 0 Yes 1 7 1 5 7
EGADS : 11 0 Yes 3 8 1 5 6
EGADS : 12 0 Yes 7 8 1 5 8
EGADS : 13 0 Yes 5 9 1 6 7
EGADS : 14 0 Yes 8 9 1 6 8
EGADS : 15 0 Yes 9 7 1 7 8
EGADS : 16 1 Yes 10 11 1 9 11
EGADS : 17 1 Yes 10 12 1 9 13
EGADS : 18 1 Yes 12 13 1 9 10
EGADS : 19 1 Yes 11 13 1 9 12
EGADS : 20 1 Yes 12 14 1 10 14
EGADS : 21 1 Yes 14 15 1 10 11
EGADS : 22 1 Yes 13 15 1 10 12
EGADS : 23 1 Yes 14 10 1 11 15
EGADS : 24 1 Yes 15 11 1 11 12
EGADS : 25 1 Yes 10 16 1 13 15
EGADS : 26 1 Yes 12 17 1 13 14
EGADS : 27 1 Yes 16 17 1 13 16
EGADS : 28 1 Yes 14 18 1 14 15
EGADS : 29 1 Yes 17 18 1 14 16
EGADS : 30 1 Yes 18 16 1 15 16
EGADS : 31 2 DEGEN 19 19 - 17
EGADS : 32 2 Yes 20 19 NA 17 18
EGADS : 33 2 DEGEN 20 20 - 17
EGADS : 34 2 Yes 20 19 NA 17 18
EGADS : 35 2 DEGEN 19 19 - 18
EGADS : 36 2 DEGEN 20 20 - 18
EGADS : Node Information
EGADS : Node Active Coordinates
EGADS : 1 Yes 3.77246052 0 0.00459131419
EGADS : 2 Yes 5.90487498 7.07106781 0
EGADS : 3 Yes 0 0 0
EGADS : 4 Yes 4.0824829 7.07106781 0.123425948
EGADS : 5 Yes 3.77001182 0 0
EGADS : 6 Yes 5.90282524 7.07106781 0
EGADS : 7 Yes 5.90487498 0 0
EGADS : 8 Yes 4.0824829 0 0.123425948
EGADS : 9 Yes 5.90282524 0 0
EGADS : 10 Yes 11.5089842 0 0.00183652568
EGADS : 11 Yes 12.36195 2.82842712 0
EGADS : 12 Yes 10 0 0
EGADS : 13 Yes 11.6329932 2.82842712 0.0493703791
EGADS : 14 Yes 11.5080047 0 0
EGADS : 15 Yes 12.3611301 2.82842712 0
EGADS : 16 Yes 12.36195 0 0
EGADS : 17 Yes 11.6329932 0 0.0493703791
EGADS : 18 Yes 12.3611301 0 0
EGADS : 19 Yes 0 0 80
EGADS : 20 Yes 0 0 0
EGADS : Face and Edge Match Information
EGADS : No Face Matches Found
AFLR4 : Surface Mesh Spacing Setup
AFLR4 : Max Bounding Box Length = 160
AFLR4 : Min Bounding Box Length = 160
AFLR4 : Max Ref Bounding Box Length = 14.1421
AFLR4 : Min Ref Bounding Box Length = 0.890888
AFLR4 : Reference Length = 0.890888
AFLR4 : BL Thickness = 0
AFLR4 : FarField Spacing = 15.6122
AFLR4 : Abs Min Surf Spacing = 0.00222722
AFLR4 : Min Surf Spacing = 0.00445444
AFLR4 : Max Surf Spacing = 0.0890888
AFLR4 : Global Scale Factor = 1
AFLR4 : Geometry Definition Information
AFLR4 : Definition Definition Composite Grid BC
AFLR4 : ID Type ID Type
AFLR4 : 0 glue-only composite - -
AFLR4 : 1 CAD geometry 0 STD
AFLR4 : 2 CAD geometry 0 STD
AFLR4 : 3 CAD geometry 0 STD
AFLR4 : 4 CAD geometry 0 STD
AFLR4 : 5 CAD geometry 0 STD
AFLR4 : 6 CAD geometry 0 STD
AFLR4 : 7 CAD geometry 0 STD
AFLR4 : 8 CAD geometry 0 STD
AFLR4 : 9 CAD geometry 0 STD
AFLR4 : 10 CAD geometry 0 STD
AFLR4 : 11 CAD geometry 0 STD
AFLR4 : 12 CAD geometry 0 STD
AFLR4 : 13 CAD geometry 0 STD
AFLR4 : 14 CAD geometry 0 STD
AFLR4 : 15 CAD geometry 0 STD
AFLR4 : 16 CAD geometry 0 STD
AFLR4 : 17 CAD geometry 0 FARFIELD
AFLR4 : 18 CAD geometry 0 FARFIELD
AFLR4 : Case has 2 Proximity Checking Components
AFLR4 : Component 1 includes Definitions 1 2 3 4 5 6 7 8
AFLR4 : Component 2 includes Definitions 9 10 11 12 13 14 15 16
AFLR4 : Define CAD surface definition 1
AFLR4 : Define CAD surface definition 2
AFLR4 : Define CAD surface definition 3
AFLR4 : Define CAD surface definition 4
AFLR4 : Define CAD surface definition 5
AFLR4 : Define CAD surface definition 6
AFLR4 : Define CAD surface definition 7
AFLR4 : Define CAD surface definition 8
AFLR4 : Define CAD surface definition 9
AFLR4 : Define CAD surface definition 10
AFLR4 : Define CAD surface definition 11
AFLR4 : Define CAD surface definition 12
AFLR4 : Define CAD surface definition 13
AFLR4 : Define CAD surface definition 14
AFLR4 : Define CAD surface definition 15
AFLR4 : Define CAD surface definition 16
AFLR4 : Define CAD surface definition 17
AFLR4 : Define CAD surface definition 18
AFLR43 : INPUT SURFACE MESH FROM TESS
AFLR43 : Quad Surface Faces= 0
AFLR43 : Tria Surface Faces= 12428
AFLR43 : Nodes = 6220
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
UG PARAM : mrecm = 3
UG PARAM : mrecqm = 3
UG PARAM : mpfrmt = 0
AFLR3 : ---------------------------------------
AFLR3 : AFLR3 LIBRARY
AFLR3 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3 : TETRAHEDRAL GRID GENERATOR
AFLR3 : Version Number 16.32.50
AFLR3 : Version Date 10/31/23 @ 06:31PM
AFLR3 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR3 : Compile Date 03/08/24 @ 01:03AM
AFLR3 : Copyright 1994-2021, D.L. Marcum
AFLR3 : ---------------------------------------
AFLR3 IC : INPUT SURFACE GRID CHECK
AFLR3 IC : Nodes, Elements = 6220 0
UG3 : Boundary Conditions
UG3 : B-Face ID Boundary Condition
UG3 : 1 Solid
UG3 : 2 Solid
UG3 : 3 Solid
UG3 : 4 Solid
UG3 : 5 Solid
UG3 : 6 Solid
UG3 : 7 Solid
UG3 : 8 Solid
UG3 : 9 Solid
UG3 : 10 Solid
UG3 : 11 Solid
UG3 : 12 Solid
UG3 : 13 Solid
UG3 : 14 Solid
UG3 : 15 Solid
UG3 : 16 Solid
UG3 : 17 FarField
UG3 : 18 FarField
AFLR3 : CPU Time = 0.017 seconds
AFLR3 IG : INITIAL VOLUME GRID GENERATION
AFLR3 IG : Nodes, Elements = 6220 0
AFLR3 IG : Nodes, Elements = 8 10
AFLR3 IG : Nodes, Elements = 1246 7333
AFLR3 IG : Nodes, Elements = 2492 16261
AFLR3 IG : Nodes, Elements = 3738 25021
AFLR3 IG : Nodes, Elements = 4984 34304
AFLR3 IG : Nodes, Elements = 6227 43518
AFLR3 IG : Nodes, Elements = 6227 43440
AFLR3 IG : Nodes, Elements = 6227 43475
AFLR3 IG : Nodes, Elements = 6227 43439
AFLR3 IG : Nodes, Elements = 6220 26110
AFLR3 IG : Nodes, Elements = 6220 26133
AFLR3 IG : Nodes, Elements = 6220 21488
AFLR3 IG : Nodes, Elements = 6220 19195
AFLR3 : CPU Time = 0.229 seconds
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
AFLR3 GG : Nodes, Elements = 6220 19195
AFLR3 GG : Nodes, Elements = 9104 28052
AFLR3 GG : Nodes, Elements = 9104 39102
AFLR3 GG : Nodes, Elements = 9104 36335
AFLR3 GG : Nodes, Elements = 9104 34880
AFLR3 GG : Nodes, Elements = 11662 42890
AFLR3 GG : Nodes, Elements = 11662 54004
AFLR3 GG : Nodes, Elements = 11662 50843
AFLR3 GG : Nodes, Elements = 11662 49925
AFLR3 GG : Nodes, Elements = 14498 58736
AFLR3 GG : Nodes, Elements = 14498 71038
AFLR3 GG : Nodes, Elements = 14498 67638
AFLR3 GG : Nodes, Elements = 14498 66762
AFLR3 GG : Nodes, Elements = 17480 75922
AFLR3 GG : Nodes, Elements = 17480 88720
AFLR3 GG : Nodes, Elements = 17480 85188
AFLR3 GG : Nodes, Elements = 17480 84349
AFLR3 GG : Nodes, Elements = 20711 94213
AFLR3 GG : Nodes, Elements = 20711 107855
AFLR3 GG : Nodes, Elements = 20711 104214
AFLR3 GG : Nodes, Elements = 20711 103375
AFLR3 GG : Nodes, Elements = 24093 113678
AFLR3 GG : Nodes, Elements = 24093 128254
AFLR3 GG : Nodes, Elements = 24093 124257
AFLR3 GG : Nodes, Elements = 24093 123406
AFLR3 GG : Nodes, Elements = 27618 134141
AFLR3 GG : Nodes, Elements = 27618 149080
AFLR3 GG : Nodes, Elements = 27618 145168
AFLR3 GG : Nodes, Elements = 27618 144374
AFLR3 GG : Nodes, Elements = 31189 155227
AFLR3 GG : Nodes, Elements = 31189 170286
AFLR3 GG : Nodes, Elements = 31189 166309
AFLR3 GG : Nodes, Elements = 31189 165453
AFLR3 GG : Nodes, Elements = 34751 176284
AFLR3 GG : Nodes, Elements = 34751 191463
AFLR3 GG : Nodes, Elements = 34751 187411
AFLR3 GG : Nodes, Elements = 34751 186588
AFLR3 GG : Nodes, Elements = 38283 197293
AFLR3 GG : Nodes, Elements = 38283 212453
AFLR3 GG : Nodes, Elements = 38283 208438
AFLR3 GG : Nodes, Elements = 38283 207716
AFLR3 GG : Nodes, Elements = 41833 218438
AFLR3 GG : Nodes, Elements = 41833 233399
AFLR3 GG : Nodes, Elements = 41833 229556
AFLR3 GG : Nodes, Elements = 41833 228802
AFLR3 GG : Nodes, Elements = 45233 239061
AFLR3 GG : Nodes, Elements = 45233 253453
AFLR3 GG : Nodes, Elements = 45233 249686
AFLR3 GG : Nodes, Elements = 45233 248980
AFLR3 GG : Nodes, Elements = 48547 258960
AFLR3 GG : Nodes, Elements = 48547 273037
AFLR3 GG : Nodes, Elements = 48547 269340
AFLR3 GG : Nodes, Elements = 48547 268660
AFLR3 GG : Nodes, Elements = 51788 278411
AFLR3 GG : Nodes, Elements = 51788 292195
AFLR3 GG : Nodes, Elements = 51788 288655
AFLR3 GG : Nodes, Elements = 51788 288020
AFLR3 GG : Nodes, Elements = 54897 297367
AFLR3 GG : Nodes, Elements = 54897 310536
AFLR3 GG : Nodes, Elements = 54897 307175
AFLR3 GG : Nodes, Elements = 54897 306599
AFLR3 GG : Nodes, Elements = 57861 315502
AFLR3 GG : Nodes, Elements = 57861 327967
AFLR3 GG : Nodes, Elements = 57861 324838
AFLR3 GG : Nodes, Elements = 57861 324290
AFLR3 GG : Nodes, Elements = 60791 333083
AFLR3 GG : Nodes, Elements = 60791 345364
AFLR3 GG : Nodes, Elements = 60791 342206
AFLR3 GG : Nodes, Elements = 60791 341750
AFLR3 GG : Nodes, Elements = 63489 349850
AFLR3 GG : Nodes, Elements = 63489 361174
AFLR3 GG : Nodes, Elements = 63489 358324
AFLR3 GG : Nodes, Elements = 63489 357881
AFLR3 GG : Nodes, Elements = 65986 365375
AFLR3 GG : Nodes, Elements = 65986 375877
AFLR3 GG : Nodes, Elements = 65986 373150
AFLR3 GG : Nodes, Elements = 65986 372801
AFLR3 GG : Nodes, Elements = 68262 379634
AFLR3 GG : Nodes, Elements = 68262 389039
AFLR3 GG : Nodes, Elements = 68262 386682
AFLR3 GG : Nodes, Elements = 68262 386428
AFLR3 GG : Nodes, Elements = 70242 392370
AFLR3 GG : Nodes, Elements = 70242 400574
AFLR3 GG : Nodes, Elements = 70242 398524
AFLR3 GG : Nodes, Elements = 70242 398290
AFLR3 GG : Nodes, Elements = 71834 403067
AFLR3 GG : Nodes, Elements = 71834 409901
AFLR3 GG : Nodes, Elements = 71834 408035
AFLR3 GG : Nodes, Elements = 71834 407840
AFLR3 GG : Nodes, Elements = 73096 411631
AFLR3 GG : Nodes, Elements = 73096 416942
AFLR3 GG : Nodes, Elements = 73096 415543
AFLR3 GG : Nodes, Elements = 73096 415387
AFLR3 GG : Nodes, Elements = 74042 418225
AFLR3 GG : Nodes, Elements = 74042 422196
AFLR3 GG : Nodes, Elements = 74042 421120
AFLR3 GG : Nodes, Elements = 74042 421030
AFLR3 GG : Nodes, Elements = 74697 422995
AFLR3 GG : Nodes, Elements = 74697 425691
AFLR3 GG : Nodes, Elements = 74697 424979
AFLR3 GG : Nodes, Elements = 74697 424921
AFLR3 GG : Nodes, Elements = 75147 426271
AFLR3 GG : Nodes, Elements = 75147 428179
AFLR3 GG : Nodes, Elements = 75147 427658
AFLR3 GG : Nodes, Elements = 75147 427613
AFLR3 GG : Nodes, Elements = 75442 428499
AFLR3 GG : Nodes, Elements = 75442 429739
AFLR3 GG : Nodes, Elements = 75442 429380
AFLR3 GG : Nodes, Elements = 75442 429354
AFLR3 GG : Nodes, Elements = 75634 429930
AFLR3 GG : Nodes, Elements = 75634 430753
AFLR3 GG : Nodes, Elements = 75634 430521
AFLR3 GG : Nodes, Elements = 75634 430497
AFLR3 GG : Nodes, Elements = 75743 430824
AFLR3 GG : Nodes, Elements = 75743 431284
AFLR3 GG : Nodes, Elements = 75743 431147
AFLR3 GG : Nodes, Elements = 75743 431140
AFLR3 GG : Nodes, Elements = 75813 431351
AFLR3 GG : Nodes, Elements = 75813 431632
AFLR3 GG : Nodes, Elements = 75813 431554
AFLR3 GG : Nodes, Elements = 75813 431549
AFLR3 GG : Nodes, Elements = 75854 431672
AFLR3 GG : Nodes, Elements = 75854 431830
AFLR3 GG : Nodes, Elements = 75854 431793
AFLR3 GG : Nodes, Elements = 75854 431785
AFLR3 GG : Nodes, Elements = 75878 431857
AFLR3 GG : Nodes, Elements = 75878 431960
AFLR3 GG : Nodes, Elements = 75878 431923
AFLR3 GG : Nodes, Elements = 75878 431919
AFLR3 GG : Nodes, Elements = 75896 431973
AFLR3 GG : Nodes, Elements = 75896 432050
AFLR3 GG : Nodes, Elements = 75896 432029
AFLR3 GG : Nodes, Elements = 75896 432027
AFLR3 GG : Nodes, Elements = 75911 432072
AFLR3 GG : Nodes, Elements = 75911 432140
AFLR3 GG : Nodes, Elements = 75911 432115
AFLR3 GG : Nodes, Elements = 75911 432113
AFLR3 GG : Nodes, Elements = 75917 432131
AFLR3 GG : Nodes, Elements = 75917 432161
AFLR3 GG : Nodes, Elements = 75917 432148
AFLR3 GG : Nodes, Elements = 75917 432146
AFLR3 GG : Nodes, Elements = 75922 432161
AFLR3 GG : Nodes, Elements = 75922 432186
AFLR3 GG : Nodes, Elements = 75922 432175
AFLR3 GG : Nodes, Elements = 75925 432184
AFLR3 GG : Nodes, Elements = 75925 432192
AFLR3 GG : Nodes, Elements = 75925 432191
AFLR3 GG : Nodes, Elements = 75927 432197
AFLR3 GG : Nodes, Elements = 75927 432207
AFLR3 GG : Nodes, Elements = 75927 432204
AFLR3 GG : Nodes, Elements = 75929 432210
AFLR3 GG : Nodes, Elements = 75929 432216
AFLR3 GG : Nodes, Elements = 75929 432215
AFLR3 GG : Nodes, Elements = 75932 432224
AFLR3 GG : Nodes, Elements = 75932 432240
AFLR3 GG : Nodes, Elements = 75932 432234
AFLR3 GG : Nodes, Elements = 75932 432233
AFLR3 GG : Nodes, Elements = 75933 432236
AFLR3 GG : Nodes, Elements = 75933 432244
AFLR3 GG : Nodes, Elements = 75933 432241
AFLR3 GG : Nodes, Elements = 75933 432240
AFLR3 GG : Nodes, Elements = 75962 432327
AFLR3 GG : Nodes, Elements = 75962 432440
AFLR3 GG : Nodes, Elements = 75962 432401
AFLR3 GG : Nodes, Elements = 75962 432400
AFLR3 GG : Nodes, Elements = 75964 432406
AFLR3 GG : Nodes, Elements = 75964 432411
AFLR3 GG : Nodes, Elements = 75964 432408
AFLR3 : CPU Time = 7.587 seconds
AFLR3 QI : QUALITY IMPROVEMENT
AFLR3 QI : Nodes, Elements = 75964 432408
AFLR3 QI : Nodes, Elements = 74464 423905
AFLR3 QI : Nodes, Elements = 74236 422620
AFLR3 QI : Nodes, Elements = 74218 422515
AFLR3 QI : Nodes, Elements = 74218 426676
AFLR3 QI : Nodes, Elements = 74218 422354
AFLR3 QI : Nodes, Elements = 74218 421937
AFLR3 QI : Nodes, Elements = 74218 422317
AFLR3 QI : Nodes, Elements = 74218 421673
AFLR3 QI : Nodes, Elements = 74218 421449
AFLR3 QI : Nodes, Elements = 74218 421720
AFLR3 QI : Nodes, Elements = 74218 421413
AFLR3 QI : Nodes, Elements = 74218 421313
AFLR3 QI : Nodes, Elements = 74218 421535
AFLR3 QI : Nodes, Elements = 74218 421304
AFLR3 QI : Nodes, Elements = 74218 421266
AFLR3 QI : Nodes, Elements = 74218 421471
AFLR3 QI : Nodes, Elements = 74218 421263
AFLR3 QI : Nodes, Elements = 74218 421232
AFLR3 QI : Nodes, Elements = 74223 421255
AFLR3 QI : Nodes, Elements = 74223 421470
AFLR3 QI : Nodes, Elements = 74223 421272
AFLR3 QI : Nodes, Elements = 74223 421260
AFLR3 QI : Nodes, Elements = 74223 421451
AFLR3 QI : Nodes, Elements = 74223 421266
AFLR3 QI : Nodes, Elements = 74223 421234
AFLR3 : CPU Time = 2.372 seconds
AFLR3 QRG: QUALITY GRID RE-GENERATION
AFLR3 QRG: Nodes, Elements = 74223 421234
AFLR3 QRG: Nodes, Elements = 74223 421233
AFLR3 QRG: Nodes, Elements = 74223 421232
AFLR3 QRG: Nodes, Elements = 74225 421243
AFLR3 QRG: Nodes, Elements = 74230 421269
AFLR3 QRG: Nodes, Elements = 74239 421316
AFLR3 : CPU Time = 0.116 seconds
AFLR3 : DONE
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Ang = 1.064 171.4
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 62
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 421316
UG3 : Min Vol = 6.77e-10
UG3 : Average Vol = 5.04
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 = 421316
UG3 : Min, Max Q = 0.0787 1
UG3 : Average Q = 0.894
UG3 : No. Q< 0.1 = 24
UG3 : No. Q< 0.01 = 0
OVERALL : CPU Time = 10.685 seconds
UG3 : DIHEDRAL ANGLE CHECK
UG3 : No. Tet Elems = 421316
UG3 : Min, Max Ang = 1.064 171.4
UG3 : Average Angle = 70.2
UG3 : No. Angle>160.0 = 62
UG3 : No. Angle>179.9 = 0
UG3 : VOL CHECK
UG3 : Total-Volume = 2.12e+06
UG3 : No. Tet Elems = 421316
UG3 : Min Vol = 6.77e-10
UG3 : Average Vol = 5.04
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 = 421316
UG3 : Min, Max Q = 0.188 1
UG3 : Average Q = 0.854
UG3 : No. Q< 0.1 = 0
UG3 : No. Q< 0.01 = 0
UG3 : CPU Time = 0.000 seconds
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : CREATE EGADS TESS FROM AFLR3 DATA
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 1
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 2
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 3
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 4
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 5
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 6
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 7
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 8
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 9
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 10
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 11
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 12
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 13
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 14
EGADS : CREATING TESSELLATION FOR BODY 0 EDGE 15
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 1
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 2
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 3
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 4
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 5
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 6
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 7
EGADS : CREATING TESSELLATION FOR BODY 0 FACE 8
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 16
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 17
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 18
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 19
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 20
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 21
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 22
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 23
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 24
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 25
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 26
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 27
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 28
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 29
EGADS : CREATING TESSELLATION FOR BODY 1 EDGE 30
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 9
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 10
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 11
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 12
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 13
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 14
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 15
EGADS : CREATING TESSELLATION FOR BODY 1 FACE 16
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 32
EGADS : CREATING TESSELLATION FOR BODY 2 EDGE 34
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 17
EGADS : CREATING TESSELLATION FOR BODY 2 FACE 18
EGADS : EGADS TESS CREATED
EGADS : CHECK TESS FACE NODE MAP
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 1
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 2
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 3
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 4
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 5
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 6
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 7
EGADS : CHECKING NODE MAP FOR BODY 0 FACE 8
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 9
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 10
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 11
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 12
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 13
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 14
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 15
EGADS : CHECKING NODE MAP FOR BODY 1 FACE 16
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 17
EGADS : CHECKING NODE MAP FOR BODY 2 FACE 18
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Cardinal"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Raven"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Falcon"
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 1
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.5.1) "
ok
test_invalidBoundary (test_su2.TestSU2.test_invalidBoundary) ... Getting CFD boundary conditions
Boundary condition name - Wing1
ok
test_invalidBoundaryName (test_su2.TestSU2.test_invalidBoundaryName) ... Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - X
ok
test_journal (test_su2.TestSU2.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 1
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
Running SU2 2
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
Number of pyramids = 0
Number of prisms = 0
Number of hexahedrals = 0
Writing SU2 file ....
Finished writing SU2 file
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 1
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
Writing boundary flags
- bcProps.surfaceProp[0].surfaceType = 3
- bcProps.surfaceProp[1].surfaceType = 2
- bcProps.surfaceProp[2].surfaceType = 1
Done boundary flags
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "Harrier (8.0.1)"
CAPS Info: Hit last success -- going live!
Running SU2 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting CFD boundary conditions
Boundary condition name - Farfield
Boundary condition name - Wing1
Boundary condition name - Wing2
Done getting CFD boundary conditions
ok
test_phase (test_su2.TestSU2.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
AFLR4 : Proximity BG Surface Grid Generation Skipped
AFLR4 : No Modifications Required
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 3
Name = Wing1, index = 1
Name = Wing2, index = 2
Name = Farfield, index = 3
Getting volume mesh
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 74239
Number of elements = 433744
Number of triangles = 12428
Number of quadrilatarals = 0
Number of tetrahedrals = 421316
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:62030)
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)
7FEF5D466700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
7FEF7FA4A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
7FEF7FA4A740 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
7FEF5D466700 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
Getting surface mesh for body 7 (of 7)
Body 1 (of 7)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 2 (of 7)
Number of nodes = 296
Number of elements = 588
Number of triangle elements = 588
Number of quadrilateral elements = 0
Body 3 (of 7)
Number of nodes = 487
Number of elements = 970
Number of triangle elements = 970
Number of quadrilateral elements = 0
Body 4 (of 7)
Number of nodes = 2048
Number of elements = 4096
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Body 5 (of 7)
Number of nodes = 152
Number of elements = 300
Number of triangle elements = 300
Number of quadrilateral elements = 0
Body 6 (of 7)
Number of nodes = 624
Number of elements = 1248
Number of triangle elements = 1248
Number of quadrilateral elements = 0
Body 7 (of 7)
Number of nodes = 488
Number of elements = 972
Number of triangle elements = 972
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 4193
Total number of elements = 8366
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh for body 1 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = box, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cylinder, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = cone, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = torus, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = sphere, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 6 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = boxhole, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 7 (of 7)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = bullet, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Body 1 number of surface: nodes - 98, elements - 192
Body 2 number of surface: nodes - 296, elements - 588
Body 3 number of surface: nodes - 487, elements - 970
Body 4 number of surface: nodes - 2048, elements - 4096
Body 5 number of surface: nodes - 152, elements - 300
Body 6 number of surface: nodes - 624, elements - 1248
Body 7 number of surface: nodes - 488, elements - 972
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 7
Name = box, index = 1
Name = cylinder, index = 2
Name = cone, index = 3
Name = torus, index = 4
Name = sphere, index = 5
Name = boxhole, index = 6
Name = bullet, index = 7
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of surface: nodes - 4193, elements - 8366
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_faceMatch_MultiDomain (test_tetgen.TestTETGEN.test_faceMatch_MultiDomain) ... ../csmData/MultiDomain/example1.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 374
Number of elements = 744
Number of triangle elements = 744
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 472
Total number of elements = 936
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 374, elements - 744
Body 2 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example2.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 386
Number of elements = 768
Number of triangle elements = 768
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 582
Total number of elements = 1152
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 386, elements - 768
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 98, elements - 192
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example3.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 351
Number of elements = 698
Number of triangle elements = 698
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 491
Total number of elements = 970
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 351, elements - 698
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example4.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 376
Number of elements = 748
Number of triangle elements = 748
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 98
Number of elements = 192
Number of triangle elements = 192
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1020
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 376, elements - 748
Body 2 number of surface: nodes - 98, elements - 192
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example6.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 42
Number of elements = 80
Number of triangle elements = 80
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 454
Total number of elements = 896
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 42, elements - 80
Body 3 number of surface: nodes - 42, elements - 80
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example7.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 370
Number of elements = 736
Number of triangle elements = 736
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 126
Number of elements = 252
Number of triangle elements = 252
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 20
Number of elements = 36
Number of triangle elements = 36
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 516
Total number of elements = 1024
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 370, elements - 736
Body 2 number of surface: nodes - 126, elements - 252
Body 3 number of surface: nodes - 20, elements - 36
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example8.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 3)
Getting surface mesh for body 2 (of 3)
Getting surface mesh for body 3 (of 3)
Body 1 (of 3)
Number of nodes = 109
Number of elements = 214
Number of triangle elements = 214
Number of quadrilateral elements = 0
Body 2 (of 3)
Number of nodes = 48
Number of elements = 96
Number of triangle elements = 96
Number of quadrilateral elements = 0
Body 3 (of 3)
Number of nodes = 12
Number of elements = 20
Number of triangle elements = 20
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 169
Total number of elements = 330
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 109, elements - 214
Body 2 number of surface: nodes - 48, elements - 96
Body 3 number of surface: nodes - 12, elements - 20
Getting volume mesh for body 1 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 3)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/example9.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 536
Number of elements = 1072
Number of triangle elements = 1072
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 544
Number of elements = 1084
Number of triangle elements = 1084
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 1080
Total number of elements = 2156
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 536, elements - 1072
Body 2 number of surface: nodes - 544, elements - 1084
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/multi_prim.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 5)
Getting surface mesh for body 2 (of 5)
Getting surface mesh for body 3 (of 5)
Getting surface mesh for body 4 (of 5)
Getting surface mesh for body 5 (of 5)
Body 1 (of 5)
Number of nodes = 1352
Number of elements = 2684
Number of triangle elements = 2684
Number of quadrilateral elements = 0
Body 2 (of 5)
Number of nodes = 288
Number of elements = 572
Number of triangle elements = 572
Number of quadrilateral elements = 0
Body 3 (of 5)
Number of nodes = 173
Number of elements = 342
Number of triangle elements = 342
Number of quadrilateral elements = 0
Body 4 (of 5)
Number of nodes = 26
Number of elements = 48
Number of triangle elements = 48
Number of quadrilateral elements = 0
Body 5 (of 5)
Number of nodes = 482
Number of elements = 960
Number of triangle elements = 960
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 2321
Total number of elements = 4606
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 1352, elements - 2684
Body 2 number of surface: nodes - 288, elements - 572
Body 3 number of surface: nodes - 173, elements - 342
Body 4 number of surface: nodes - 26, elements - 48
Body 5 number of surface: nodes - 482, elements - 960
Getting volume mesh for body 1 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 3 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 4 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 5 (of 5)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
../csmData/MultiDomain/cyl_seam.csm
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
Getting surface mesh for body 2 (of 2)
Body 1 (of 2)
Number of nodes = 440
Number of elements = 876
Number of triangle elements = 876
Number of quadrilateral elements = 0
Body 2 (of 2)
Number of nodes = 522
Number of elements = 1044
Number of triangle elements = 1044
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 962
Total number of elements = 1920
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Body 1 number of surface: nodes - 440, elements - 876
Body 2 number of surface: nodes - 522, elements - 1044
Getting volume mesh for body 1 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Getting volume mesh for body 2 (of 2)
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 1
Name = dummy_att, index = 1
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_journal (test_tetgen.TestTETGEN.test_journal) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
CAPS Info: Hit last success -- going live!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
CAPS Info: Hit last success -- going live!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
ok
test_phase (test_tetgen.TestTETGEN.test_phase) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 7130, elements - 14252
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
ok
test_reenter (test_tetgen.TestTETGEN.test_reenter) ... Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 3
Name = Farfield, index = 1
Name = Wing1, index = 2
Name = trailingEdge, index = 3
Getting mesh sizing parameters
Mesh sizing name - Farfield
Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
Body 1 (of 1)
Number of nodes = 9626
Number of elements = 19244
Number of triangle elements = 19244
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9626
Total number of elements = 19244
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 2
Name = Farfield, index = 1
Name = Wing1, index = 2
Number of surface: nodes - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq1.500/0.000QT1.00e-16A
Done meshing using TetGen!
Writing 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 - 9626, elements - 19244
Getting volume mesh
Generating volume mesh using TetGen.....
Tetgen input string = pYq2.000/0.000QT1.00e-16A
Done meshing using TetGen!
Writing 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_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 144 tests in 527.340s
OK (skipped=26)
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/
+ make test TYPE=MINIMAL
(make -C cCAPS -f aeroelastic_SU2.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `aeroelasticSimple_Iterative_SU2_and_MystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f avlTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `avlTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f awaveTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `awaveTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f frictionTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `frictionTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f fun3d.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: Nothing to be done for `fun3d'.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f hsm.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `hsm' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f interferenceTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `interferenceTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f msesTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `msesTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f mystran.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `mystranTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
(make -C cCAPS -f pointwiseTest.make)
make[1]: Entering directory `/home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/cCAPS'
make[1]: `pointwiseTest' is up to date.
make[1]: Leaving directory `/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/ESP_venv/bin/python
=================================================
Running.... MINIMAL PyTests
=================================================
+ echo 'avl_PyTest.py test;'
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 0m0.829s
user 0m0.616s
sys 0m0.467s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -outLevel=0 -noPlotData
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
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 0m4.735s
user 0m4.621s
sys 0m0.335s
+ 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/7.8/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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Cl = 0.37837910855492407
Cd = 0.007775858417210143
Cm = 0.005262636995811319
real 0m5.551s
user 0m5.276s
sys 0m0.369s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ python -u friction_PyTest.py -outLevel=0
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 0m1.491s
user 0m0.424s
sys 0m0.187s
+ status=0
+ set +x
=================================================
CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================
=================================================
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
+ echo 'tsfoil_PyTest.py test;'
tsfoil_PyTest.py test;
+ python -u tsfoil_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 0m0.561s
user 0m0.431s
sys 0m0.217s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
delaundo_PyTest.py test;
+ python -u delaundo_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
Number of unique capsGroup attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Mapping capsMesh attributes ................
Number of unique capsMesh attributes = 6
Name = 2DSlice, index = 1
Name = TunnelWall, index = 2
Name = OutFlow, index = 3
Name = InFlow, index = 4
Name = Airfoil, index = 5
Name = AirfoilTE, index = 6
Getting mesh sizing parameters
Mesh sizing name - Airfoil
Mesh sizing name - AirfoilTE
Mesh sizing name - InFlow
Mesh sizing name - OutFlow
Mesh sizing name - TunnelWall
Done getting mesh sizing parameters
Getting edge discretization for body 1
Delaundo expects 2D meshes in the x-y plane... attempting to rotate mesh through node swapping!
Swapping z and y coordinates!
Writing delaundo control file - delaundo.ctr
Writing out *.pts file
Reading delaundo mesh file - delaundo_CAPS.mesh
Swapping y and z coordinates!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
Writing ugrid file ....
Finished writing ugrid file
real 0m0.701s
user 0m0.623s
sys 0m0.410s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
egadsTess_PyTest.py test;
+ python -u egadsTess_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 0m6.461s
user 0m13.281s
sys 0m1.373s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
aflr2_PyTest.py test;
+ python -u aflr2_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 344 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 344 344
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 70 142
AFLR2 IG : Nodes, Faces = 140 282
AFLR2 IG : Nodes, Faces = 210 422
AFLR2 IG : Nodes, Faces = 280 562
AFLR2 IG : Nodes, Faces = 316 634
AFLR2 IG : Nodes, Faces = 344 690
AFLR2 IG : Nodes, Faces = 348 690
AFLR2 IG : Nodes, Faces = 344 344
AFLR2 : CPU Time = 0.001 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 344 344
AFLR2 GGp: Nodes, Faces = 681 1018
AFLR2 GGp: Nodes, Faces = 1013 1682
AFLR2 GGp: Nodes, Faces = 1339 2334
AFLR2 GGp: Nodes, Faces = 1652 2960
AFLR2 GGp: Nodes, Faces = 1957 3570
AFLR2 GGp: Nodes, Faces = 2252 4160
AFLR2 GGp: Nodes, Faces = 2526 4708
AFLR2 GGp: Nodes, Faces = 2809 5274
AFLR2 GGp: Nodes, Faces = 3083 5822
AFLR2 GGp: Nodes, Faces = 3327 6310
AFLR2 GGp: Nodes, Faces = 3564 6784
AFLR2 GGp: Nodes, Faces = 3788 7232
AFLR2 GGp: Nodes, Faces = 3995 7646
AFLR2 GGp: Nodes, Faces = 4194 8044
AFLR2 GGp: Nodes, Faces = 4394 8444
AFLR2 GGp: Nodes, Faces = 4585 8826
AFLR2 GGp: Nodes, Faces = 4772 9200
AFLR2 GGp: Nodes, Faces = 4943 9542
AFLR2 GGp: Nodes, Faces = 5129 9914
AFLR2 GGp: Nodes, Faces = 5293 10242
AFLR2 GGp: Nodes, Faces = 5447 10550
AFLR2 GGp: Nodes, Faces = 5594 10844
AFLR2 GGp: Nodes, Faces = 5716 11088
AFLR2 GGp: Nodes, Faces = 5830 11316
AFLR2 GGp: Nodes, Faces = 5909 11474
AFLR2 GGp: Nodes, Faces = 5964 11584
AFLR2 GGp: Nodes, Faces = 6006 11668
AFLR2 GGp: Nodes, Faces = 6025 11706
AFLR2 GGp: Nodes, Faces = 6034 11724
AFLR2 : CPU Time = 0.029 seconds
AFLR2 QI : QUALITY IMPROVEMENT
AFLR2 QI : Nodes, Faces = 6034 11724
AFLR2 QI : Nodes, Faces = 6033 454
AFLR2 QI : Nodes, Faces = 6033 5634
AFLR2 QI : Nodes, Faces = 6033 11722
AFLR2 QI : Nodes, Faces = 6032 462
AFLR2 QI : Nodes, Faces = 6032 5629
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 456
AFLR2 QI : Nodes, Faces = 6032 5632
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6032 474
AFLR2 QI : Nodes, Faces = 6032 5623
AFLR2 QI : Nodes, Faces = 6032 11720
AFLR2 QI : Nodes, Faces = 6031 486
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 QI : Nodes, Faces = 6031 488
AFLR2 QI : Nodes, Faces = 6031 5616
AFLR2 : CPU Time = 0.013 seconds
AFLR2 : DONE
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing AFLR3 file ....
Finished writing AFLR3 file
Number of nodes = 6031
Number of elements = 6448
Number of tris = 488
Number of quad = 5616
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4722 complete [but 7915] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4741 4912 complete [but 7916] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5858 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5850 5851 complete [but 8742] (EG_makeConnect)!
EGADS Internal: Face 1, Side 5858 5851 complete [but 8791] (EG_makeConnect)!
EGADS Internal: Face 1, Side 4912 4722 complete [but 9417] (EG_makeConnect)!
Writing Tecplot file ....
Tecplot expects 2D meshes in the x-y plane... attempting to rotate mesh!
Swapping z and y coordinates!
Finished writing Tecplot file
real 0m0.940s
user 0m0.930s
sys 0m0.479s
+ 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/7.8/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/7.8/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR4 : ---------------------------------------
AFLR4 : AFLR4 LIBRARY
AFLR4 : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR4 : TRIA/QUAD SURFACE GRID GENERATOR
AFLR4 : Version Number 11.5.14
AFLR4 : Version Date 04/18/24 @ 12:45PM
AFLR4 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR4 : Compile Date 04/23/24 @ 12:17PM
AFLR4 : Copyright 1994-2021, D.L. Marcum
AFLR4 : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
EGADS : ---------------------------------------
EGADS : Engineering Geometry Aircraft Design System
EGADS : Version 1.25
EGADS : OpenCASCADE Version 7.8.0
EGADS : ---------------------------------------
Volume mesh:
Number of nodes = 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 0m16.514s
user 0m16.160s
sys 0m0.529s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
tetgen_PyTest.py test;
+ python -u tetgen_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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: 0.07
Removing exterior tetrahedra ...
Spreading region attributes.
Exterior tets removal seconds: 0
Suppressing Steiner points ...
Steiner suppression seconds: 0
Recovering Delaunayness...
Delaunay recovery seconds: 0.02
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: 0.71
Smoothing vertices...
Mesh smoothing seconds: 0.47
Improving mesh...
Mesh improvement seconds: 0.02
Jettisoning redundant points.
Writing nodes.
Writing elements.
Writing faces.
Writing edges.
Output seconds: 0
Total running seconds: 1.32
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 0m2.848s
user 0m2.799s
sys 0m0.298s
+ 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/7.8/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/7.8/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 9.17.15
AFLR2 : Version Date 04/23/24 @ 12:51AM
AFLR2 : Compile OS Linux 3.10.0-1160.88.1.el7.x86_64 x86_64
AFLR2 : Compile Date 04/23/24 @ 12:17PM
AFLR2 : Copyright 1994-2021, D.L. Marcum
AFLR2 : ---------------------------------------
AFLR2 IC : INPUT DATA CHECK
AFLR2 IC : Nodes, Faces = 545 0
AFLR2 : CPU Time = 0.000 seconds
AFLR2 EG : EDGE GRID RE-GENERATION
AFLR2 EG : Nodes, Edges = 545 545
AFLR2 : CPU Time = 0.000 seconds
AFLR2 IG : INITIAL GRID GENERATION
AFLR2 IG : Nodes, Faces = 0 2
AFLR2 IG : Nodes, Faces = 110 222
AFLR2 IG : Nodes, Faces = 220 442
AFLR2 IG : Nodes, Faces = 330 662
AFLR2 IG : Nodes, Faces = 440 882
AFLR2 IG : Nodes, Faces = 517 1036
AFLR2 IG : Nodes, Faces = 545 1092
AFLR2 IG : Nodes, Faces = 549 1092
AFLR2 IG : Nodes, Faces = 545 545
AFLR2 : CPU Time = 0.002 seconds
AFLR2 GG : FIELD GRID GENERATION
AFLR2 GGp: Nodes, Faces = 545 545
AFLR2 GGp: Nodes, Faces = 1083 1621
AFLR2 GGp: Nodes, Faces = 1616 2687
AFLR2 GGp: Nodes, Faces = 2144 3743
AFLR2 GGp: Nodes, Faces = 2661 4777
AFLR2 GGp: Nodes, Faces = 3171 5797
AFLR2 GGp: Nodes, Faces = 3672 6799
AFLR2 GGp: Nodes, Faces = 4158 7771
AFLR2 GGp: Nodes, Faces = 4653 8761
AFLR2 GGp: Nodes, Faces = 5142 9739
AFLR2 GGp: Nodes, Faces = 5608 10671
AFLR2 GGp: Nodes, Faces = 6055 11565
AFLR2 GGp: Nodes, Faces = 6482 12419
AFLR2 GGp: Nodes, Faces = 6880 13215
AFLR2 GGp: Nodes, Faces = 7257 13969
AFLR2 GGp: Nodes, Faces = 7614 14683
AFLR2 GGp: Nodes, Faces = 7947 15349
AFLR2 GGp: Nodes, Faces = 8276 16007
AFLR2 GGp: Nodes, Faces = 8575 16605
AFLR2 GGp: Nodes, Faces = 8869 17193
AFLR2 GGp: Nodes, Faces = 9140 17735
AFLR2 GGp: Nodes, Faces = 9401 18257
AFLR2 GGp: Nodes, Faces = 9654 18763
AFLR2 GGp: Nodes, Faces = 9887 19229
AFLR2 GGp: Nodes, Faces = 10110 19675
AFLR2 GGp: Nodes, Faces = 10315 20085
AFLR2 GGp: Nodes, Faces = 10497 20449
AFLR2 GGp: Nodes, Faces = 10656 20767
AFLR2 GGp: Nodes, Faces = 10791 21037
AFLR2 GGp: Nodes, Faces = 10919 21293
AFLR2 GGp: Nodes, Faces = 11022 21499
AFLR2 GGp: Nodes, Faces = 11092 21639
AFLR2 GGp: Nodes, Faces = 11145 21745
AFLR2 GGp: Nodes, Faces = 11156 21767
AFLR2 : CPU Time = 0.044 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| 1.0874e-01| 0.071067| 2.739763| 1.616077| 5.599701| 0.055267|
| 0| 0| 1| 0.0000e+00| 0.0000e+00| 1.0534e-01| -0.447576| 2.193837| 1.571349| 5.070382| 0.046028|
| 0| 0| 2| 0.0000e+00| 0.0000e+00| 1.0436e-01| -0.561159| 2.074597| 1.490746| 4.953698| 0.033910|
| 0| 0| 3| 0.0000e+00| 0.0000e+00| 1.0346e-01| -0.723326| 1.921155| 1.390756| 4.790278| 0.049695|
| 0| 0| 4| 0.0000e+00| 0.0000e+00| 1.0359e-01| -0.876572| 1.825653| 1.275093| 4.637161| 0.133976|
| 0| 0| 5| 0.0000e+00| 0.0000e+00| 1.0534e-01| -1.029177| 1.759196| 1.156078| 4.482282| 0.368542|
| 0| 0| 6| 0.0000e+00| 0.0000e+00| 1.0523e-01| -1.215334| 1.704909| 1.114966| 4.286060| 0.974759|
| 0| 0| 7| 0.0000e+00| 0.0000e+00| 1.0541e-01| -1.329970| 1.644937| 1.145030| 4.116982| 2.716332|
| 0| 0| 8| 0.0000e+00| 0.0000e+00| 1.0590e-01| -1.270672| 1.570739| 1.155400| 4.139480| 16.569216|
| 0| 0| 9| 0.0000e+00| 0.0000e+00| 1.0630e-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 0m2.413s
user 0m2.195s
sys 0m0.478s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
masstran_PyTest.py test;
+ python -u masstran_PyTest.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 0m4.710s
user 0m7.338s
sys 0m2.039s
+ 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/7.8/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/7.8/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 0m1.431s
user 0m1.383s
sys 0m0.388s
+ 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/7.8/LINUX64/EngSketchPad/CAPSexamples/regressionTest/pyCAPSlog.txt
../corsairlite/qp.py test;
+ python -u ../corsairlite/qp.py -outLevel=0
+ tee -a /home/jenkins/workspace/ESP_Beta/7.8/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 0m2.177s
user 0m2.446s
sys 0m0.733s
+ 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/7.8/LINUX64
+ mkdir -p /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ cd /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/test/plugs
+ find /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/EngSketchPad/data/Plugs -name 'plugs0*.csm'
+ sort -f
find: ‘/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/LINUX64/JenkinsESP/data/plugs/plugsFailure.txt
+ cp /home/jenkins/workspace/ESP_Beta/7.8/LINUX64/JenkinsESP/data/plugs/plugsIgnore.txt .
+ set +x
Testing CSM files:
total 28M
-rw-rw-r--. 1 jenkins jenkins 1.3M May 30 12:22 ASTRO.D01
-rw-rw-r--. 1 jenkins jenkins 316K May 30 12:22 ASTRO.IDX
-rwxrwxr-x. 1 jenkins jenkins 1.1M May 30 12:22 avl
-rwxrwxr-x. 1 jenkins jenkins 29K May 30 12:21 egads2cart
-rwxrwxr-x. 1 jenkins jenkins 114K May 30 12:23 egads2cgt
-rwxrwxr-x. 1 jenkins jenkins 46K May 30 12:23 friction
-rwxrwxr-x. 1 jenkins jenkins 8.2M May 30 12:22 mastros.exe
-rwxrwxr-x. 1 jenkins jenkins 727K May 30 12:22 mses
-rwxrwxr-x. 1 jenkins jenkins 536K May 30 12:22 mset
-rwxrwxr-x. 1 jenkins jenkins 39K May 30 12:22 phaseUtil
-rw-rw-r--. 1 jenkins jenkins 1.6K May 30 12:25 pod.egads
-rw-rw-r--. 1 jenkins jenkins 0 May 30 12:25 port7681.jrnl
-rwxrwxr-x. 1 jenkins jenkins 451K May 30 12:22 pplot
-rwxrwxr-x. 1 jenkins jenkins 405K May 30 12:22 pxplot
-rwxrwxr-x. 1 jenkins jenkins 115K May 30 12:22 sensCSM
-rwxrwxr-x. 1 jenkins jenkins 507K May 30 12:22 serveCSM
-rwxrwxr-x. 1 jenkins jenkins 449K May 30 12:22 serveESP
-rwxrwxr-x. 1 jenkins jenkins 568K May 30 12:22 Slugs
-rwxrwxr-x. 1 jenkins jenkins 169K May 30 12:22 TestFit
-rwxrwxr-x. 1 jenkins jenkins 62K May 30 12:21 vCurvature
-rwxrwxr-x. 1 jenkins jenkins 36K May 30 12:21 vGeom
-rwxrwxr-x. 1 jenkins jenkins 63K May 30 12:21 vTess
-rwxrwxr-x. 1 jenkins jenkins 12M May 30 12:21 vTesstatic
-rw-rw-r--. 1 jenkins jenkins 195K May 30 12:25 wingMultiModel.bdf
-rwxrwxr-x. 1 jenkins jenkins 1.1M May 30 12:22 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/7.8/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/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/LINUX64')
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Successfully parsed console log
[Clang] -> found 0 issues (skipped 0 duplicates)
[Clang] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/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/7.8/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] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Successfully parsed console log
[Static Analysis] -> found 0 issues (skipped 0 duplicates)
[Static Analysis] Parsing console log (workspace: '/home/jenkins/workspace/ESP_Beta/7.8/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=7.8,ESP_ARCH=LINUX64,buildnode=reynolds-centOS7 #720'.
[Checks API] No suitable checks publisher found.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: SUCCESS